STK培训教材a.ppt
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- 苦 司徒
- 6 years ago
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1 Satellite Tool Kit Satellite Tool Kit STK
2 Satellite Tool Kit STK STK STK 2
3 Satellite Tool Kit STK STK STK STK STK STK 3
4 Satellite Tool Kit STK 4
5 STK Application Class STK STK Scenario Class stkdemo Area Target Class** SearchArea Facility Class King of Prussia Planet Class Jupiter Star Class Alpha Centauri Target Class Iraq Satellite Class* Shuttle Sensor Class FieldOfView Sensor Class Uplink Sensor Class Downlink Scenario * 6 ** 5
6 STK Scenario Class StkDemo Area Target** Facility Planet Star Target Satellite Iraq WhiteSands Mars Regulus Amazonl ERSI YellowStone Park Baikonur Moon Calibration Tgt23 Sensor Class Sensor Class Sun Sensor Class SAR Track1 10Deg MinElev Uplink1 * 6 ** 6
7 STK 6 Files Edit Properties Tools Windows Help 7
8 STK 5 / RWDB / 8
9 STK 9
10 STK / /X / / 10
11 STK Geodetic Spherical Cartesian Cylindrical Geocentric -90º 90º -360º 360º AzElMask / 11
12 Ballistic STK STK 6 Great Arc 12
13 STK Basic Orbit Attitude Pass Break Mass Description Graphic Attributes, Pass, Display Times, Contours Constraints Basic, Sun, Temporal, Advanced 13
14 STK J2&J4 MSGP4 HPOP LOP 14
15 STK Great Arc Great Arc 15
16 STK 16
17 STK STK JPL DE405 Analytic / / 17
18 STK Boundary Centroid 18
19 STK Definition / / /SAR 19
20 STK Targeted Target Times- Boresight Type - Orientation Method -Az-El, Quaternion, Euler Angles, YPR About Boresight- Rotating or Hold Level 20
21 STK 2:1 21
22 STK AER / 22
23 STK AER 23
24 STK XY, XY, Interval, Polar, 90 24
25 STK Dynamic Display Strip Chart 25
26 STK / Satellite stkactivetle.sd stkactivetle.fr stlactivetle.wr / stkactivetle.om TLE stkactivetle.tce stkactivetle.gd TLE / City Facility / stkcitydb.gd stkcitydb.cd stkcitydb.cc stkfacility.fd stkfacility.cc stkfacility.gd 26
27 STK STK Keyword Groups BEGIN BEGIN Attitude END END Attitude keywords keywords NumberOfAttitudePoints) Value 3 NumberOfTorques 20 27
28 STK stk.v BEGIN AzElMask NumberOfPoints 4 BEGIN AzElMaskData END AzElMask 28
29 STK Attitude Az-El -.a.aem Custom Sensor.pattern Ephemeris.e Planetary Ephemeris Torque Color Bitmap/Pixmap Solar Flux.pe.tq /.bmp /.xpm 29
30 Satellite Tool Kit STK 30
31 STK STK HPOP LOP Lifetime 31
32 STK 32
33 STK HPOP JGM2 / 1960 Jacchia 1971 Jacchia Jacchia Roberts 1976 Standard Harris Priester / UTC TAI TDT 33
34 STK LOP 1976 J21 NASA JPL 34
35 STK Lifetime 35
36 Satellite Tool Kit STK 36
37 STK STK STK MSGP4 & TLE STK Walker 37
38 STK STK STK Lifetime LOP STK Chains Chains Connect VO STK/VO 38
39 Satellite Tool Kit STK 39
40 Satellite Tool Kit STK MSGP4 & TLE 40
41 STK STK low-earth orbit (LEO) medium-earth orbit (MEO) highly elliptical orbit (HEO) geosynchronous orbit (GEO) 41
42 STK 1 42
43 STK 1 semimajor axis apogee radius Eccentricity perigee radius apogee altitude perigee altitude Period mean motion Eccentricity Eccentricity 43
44 STK
45 STK 1 (3 ) Inclination right ascension or longitude of the ascending node RAAN argument of perigee 45
46 STK 1 Inclination right ascension or longitude of the ascending node RAAN argument of perigee 46
47 STK 1 (1 ) True Anomaly* Mean Anomaly* Eccentric Anomaly Argument of Latitude Time Past Ascending Node Time Past Perigee 47
48 6 STK 1 : 48
49 STK 1 49
50 STK 1 : Low-Earth Orbit (LEO) 1. STK Satellite Orbit Wizard Cancel LEO 2. LEO satellite Basic 3. Orbit 50
51 STK 1 Orbit Start Time Stop Time Step Size Propagator Orbit Epoch Coordinate Type Coordinate System Period Eccentricity Inclination Argument of Perigee RAAN True Anomaly 1 Jan :00: Jan :00: minute J4 1 Jan :00:00.00 Classical J minutes deg 0.0 deg 0.0 deg 0.0 deg : Semimajor Axis Period 51
52 STK 1 Low-Earth Orbit (LEO) ~ Globalstar TM ( ) Iridium ( ) 52
53 STK 1 : Medium-Earth Orbit (LEO) 1. MEO 2. MEO Basic 3. Orbit 53
54 STK 1 Orbit Start Time Stop Time Step Size Propagator Orbit Epoch Coordinate Type Coordinate System Apogee Altitude Perigee Altitude Inclination Argument of Perigee RAAN True Anomaly 1 Jan :00: Jan :00: minute J4 1 Jan :00:00.00 Classical J ,000 km 10,000 km 15 deg 0.0 deg 0.0 deg 0.0 deg : Semimajor Axis Apogee Altitude RAAN Lon. Ascn. Node (Longitude of the Ascending Node). 54
55 STK 1 Medium-Earth Orbit (MEO) MEO LEO MEO MEO Inmarsat-P ( satellites in 2 inclined planes at 10,355 km), Odyssey ( satellites in 3 inclined planes, also at 10,355 km) :
56 STK 1 : Highly Elliptical Orbit (HEO) 1. Orbit Wizard Next 2. Molniya Next HEO : Tools Orbit Wizard 56
57 STK 1 Highly Elliptical Orbit (HEO) /3 HEO Molniya,
58 STK 1 : Geostationary Orbit (GEO) 1. Satellite Tools Orbit Wizard Next Geostationary Next -80 Next Finish 2. GEO : scenario( ) 58
59 STK 1 Geosynchronous & Geostationary Orbits 1 ( ) 0 8 1/3 ( )
60 STK 1 Polar Orbit 90 LEO COSPAS- SARSAT 8, 4 SARSAT COSPAS
61 STK 1 Sun-Synchronous Orbit 1 61
62 STK 1 1. ( ) 2. Tools Report STK Report Tool Create 3. Report 4. Graph STK Graph Tool Create 5. Graph Graph 6. 62
63 STK 1 7. Shift 8. Basic 9. Kepler File Save 63
64 STK 2 MSGP4&TLE MSGP4 TLE TLE 64
65 STK 2 MSGP4&TLE MSGP4 Merged Simplified General Perturbation Merged MSGP4 Simplified General Perturbation SGP4 225 Simplified Deep Space General Perturbations SDGP4 225 MSGP4 Basic Properties MSGP4 Two Line Element TLE TLE TLE 65
66 STK 2 MSGP4 1. MSGP4 2. Properties Basic 3. Time Period Start Time Stop Time Epoch 25 Jun :00: Jun :00: Jun :00:
67 STK 2 MSGP4 4. Animation Start Time Stop Time Time Step Refresh Delta 25 Jun :00: Jun :00: seconds Change to High Speed 5. Units Distance Unit Time Unit Date Format Angle Unit Mass Unit Kilometers Seconds Gregorian UTC Degrees Kilograms 67
68 STK 2 MSGP4 MSGP4 TLE TLE TLE Auto Load File Load File Insert Auto Load Auto Load TLE 1. Satellite Orbit Wizard MSGP4-HEO 2. Basic Properties Orbit MSGP4 SSC Number TLE Options Load TLE Selection 3. Load Method Auto Load 68
69 STK 2 MSGP4 4. TLE File visible.tce TLE Selection 5. Basic Properties Orbit : Element Set TLE Delete : Auto Load TLE 69
70 STK 2 MSGP4 File Load File Load TLE Auto Load File Load 1. TLE File visible.tce TLE Selection 2. Load Method File Load 3. STK STKAllActive.tce TLE Selection 4. SSC Basic Properties 5. 70
71 STK 2 MSGP4 File Insert STK File Insert 1. LEO_Insert 2. Basic Properties Orbit MSGP4 SSC Number TLE Load TLE Selection 3. Load Method File Insert 4. landsat5mult.tce 5. TLE Selection Shift Basic Properties Orbit Element Set Number 5 TLE 71
72 STK 2 MSGP Graphics Properties Inherit Settings Show Elset Number 8. LEO_Insert Basic Properties TLE Options Load STK Jun : LEO_Insert 04:11 04:
73 STK 2 MSGP4 File Load 1. LEO_Insert Basic 5 Add 6 2. TLE Options Load TLE STK STKAllActive.tce 3. Basic Properties TLE Options Advanced Element Sets 4. Advanced 5. Advanced TLE Options Basic Properties : 2 73
74 STK 2 U.S. Space Command 8000 STK SSC TLE AGI 1. Tools Satellite Database 2. Satellite Database Common Name molniya* 3. Perform Search Satellite Database Search Results : *? 74
75 STK 2 4. Molniya 3-47 SSC #
76 STK 2 TLE TLE STK TLE STK 1. Tools Load TLE 2. Satellite Type interest.tce Two Line Element Set 3. Cross Reference stksatdb.sd Cross Reference Database 4. Open 76
77 STK 2 TLE 1. Load TLE Cross Reference Open TLE Load Results 2. ERBS SSC# Load TLE 4. : Cross Reference Database 77
78 STK 3 STK 78
79 STK 3 STK
80 STK 3 Sun_sunc 1. Sun_sync 2. Properties Basic 3. Time Period Start Time Stop Time Epoch 20 Mar :00: Mar :00: Mar :00:
81 STK 3 Sun_sunc 4. Animation Start Time Stop Time Time Step Refresh Delta 20 Mar :00: Mar :00: seconds Change to High Speed 5. Units Distance Unit Time Unit Date Format Angle Unit Mass Unit Kilometers Minutes Gregorian UTC Degrees Kilograms 81
82 STK 3 Sun_sunc 6. Property Graphics 7. Sun Lighting Subsolar Point Sunlight/Penumbra Penumbra/Umbra 8. Subsolar Point Sunlight/Penumbra YELLOW Penumbra/Umbra RED Display Altitude 0.0km 9. : Subsolar Point Sunlight/Penumbra Penumbra/Umbra 82
83 STK 3 TwoBody J2 J Orbit Wizard Sunsat Basic Properties Basic J2 Perturbation Special Options Secularly Precessing 2. 83
84 STK 3 Semimajor Axis Eccentricity Inclination Arg of Perigee RAAN True Anomaly km deg Station_Highlat 5. Basic Properties Position Latitude Longitude Altitude km 84
85 STK 3 6. Station_Lowlat Position Latitude Longitude Altitude km 7. Map Properties Map Projection Center Lon 90 deg 8. Reset
86 STK Sunsat Tools Access 2. 2 Compute Reports Access Access 2 3. Access Station_Highlat 8 Station_Lowlat 3 86
87 STK 3 4. Station_Highlat Properties Constraints Basic Min Elev 56 deg Station_Highlat Access 5. Sunsat Basic Properties Orbit Stop Time 27 Mar :00:00 6. Access File Refresh 7. Access Access Remove All 8. 87
88 STK Sunsat Graphics Properties Global Attributes Show Ground Tracks 2. Basic Properties Time Period Stop Time 20 Jun :00:00 Animation Loop at Time 20 Jun :00:00,Time Step min 3. Tools New Map Window 2:1 88
89 STK 3 4. Map Properties Map Properties Projection Perspective Projection Display type ECI Center Lat 90 Lon 0 Alt 4000km 5. Map Details Lat Spacing 15 Lon Spacing km 89
90 STK 4 STK STK 90
91 STK 4 1. SensorScen 2. Properties Basic 3. Time Period Start Time Stop Time Epoch 1 Nov :00: Nov :00: Nov :00:00.00 : 91
92 STK 4 4. Animation Start Time Stop Time Time Step Refresh Delta 1 Nov :00: Nov :00: seconds Change to High Speed 5. Units Distance Unit Time Unit Date Format Angle Unit Mass Unit Kilometers Seconds Gregorian UTC Degrees Kilograms 92
93 STK 4 6. Tools Satellite Database Satellite Database Common Name Telstar 1 Perform Search Satellite Database Search Results Telstar 1 OK Molniya Cape_Canaveral 8. Basic Properties Position Latitude Longitude Altitude km : * Telstar* Molniya* 93
94 STK Santa_Maria Position Latitude Longitude Altitude km
95 STK 4 1. Santa Maria Simple 2. Basic Definition Sensor Type Cone Angle Simple Conic Graphics Properties Projection Maximum Altitude 5000km Step Count 2 Step Count Minimum/Maximum Altitude 95
96 STK 4 4. Molniya Optical 5. Optical Basic Properties Sensor Type Cone Angle Simple Conic
97 STK 4 Access Constraints 1. Optical Tools Access Santa Maria Associated Objects Compute 2. Access Remove Access Cancel 3. Simple Access Molniya Report Access 4. Access Remove Accesses Molniya Access Simple Molniya 97
98 STK 4 Access Constraints 5. Cape Canaveral Fixed Tracking 6. Fixed Basic Properties Definition Sensor Type Cone Angle Simple Conic Pointing Pointing Type Targeted Fixed Boresight Type Available Targets Telstar Assigned Targets 8. Tracking Simple Conic Cone Angle 5.0 Targeted Telstar Tracking Boresight Type 9. Graphics Properties Blue 98
99 STK 4 Access Constraints 10. Tracking Access Telstar 11. Tracking Constraints Properties Basic Range Max 5000km 99
100 STK 4 Access Constraints 12. Max. Elevation Angle Constraints Properties Access Access 14. Cape Canaveral Fixed Graphics Properties Tracking 15. Fixed Access Telstar 16. Fixed Constraints Properties Basic Max Range 5000km 17. Max Range Maximum Azimuth Constraint 180, 100
101 STK 4 Access Constraints 18. Azimuth Access 19. Telstar Sfixed Basic Simple Conic Cone Angle 45.0 Pointing Fixed Pointing Type 20. Graphics Projection Persistence sec 21. Telstar Graphics Pass Leading/Trailing Ground Track Lead Type One Pass 22. Sfixed Graphics Projection Persistence 0 101
102 STK 4 Swath nadir alignment with ECF velocity constraint 1. Sfixed Tools Swath Swath Line Width 2 Stop Time 1 Nov :00:00.00, Swath 102
103 STK 4 2. Swath 3. SensorScen File Save 103
104 Satellite Tool Kit STK 104
105 Satellite Tool Kit STK Walker 105
106 STK 1 STK 106
107 STK 1 STK 107
108 STK 1 ReportScen 1. ReprotScen 2. Basic Properties 3. Time Period Start Time Stop Time Epoch 1 Nov :00: Nov :00: Nov :00:00.00 : Stop Time +1 day 108
109 STK 1 ReportScen 4. Animation Start Time Stop Time Time Step Refresh Delta 1 Nov :00: Nov :00: seconds Change to High Speed 5. Units Distance Unit Time Unit Date Format Angle Unit Mass Unit Kilometers Seconds Gregorian UTC Degrees Kilograms 109
110 STK 1 ReportScen Orbit Wizard Critically inclined Satrep 110
111 STK 1 1. Tools Report 2. STK Report Tool Styles LLA Position Create 111
112 STK 1 3. STK Report Tool 4. Report Tool LLA Position Time Period Report Time Periods 5. Contents Section1 Intervals Stop Time 1 Nov :00:00.00 Change 6. Use Ephemeris Steps Write Intervals to Report Step Size STK Report Tool Create STK Report Tool Time Period Stop Time 2 Nov :00:00.00 Use Ephemeris Steps 112
113 STK 1 1. Tools Report 2. STK Report Tool Styles LLA Posion Create 3. Files Units Units Use Default Report Units Unit Distance Unit Change Unit Value Nautical Miles Time Unit Seconds Hours 113
114 STK 1 1. Satrep STK Report Tool New Styles 2. Styles Quat-YPR-Euler Change 3. Properties 4. Report Style Properties Header Title Attitude Conversions Short Description Long Description 5. Content Section Line 6. Content Attitude Quaternions Attitude Quaternions Report Contents 7. New Line Line2 Report Contents! : 114
115 STK 1 8. Attitude YPR Report Contents Attitude YPR-Yaw Pitch Roll Line2 9. New Line Euler Angles Report Contents Section Quaternions YPR Euler Angles 115
116 STK 1 8. STK Report Tool Create ReportScen Files Save : Report Contents Style Properties Options Section 116
117 STK 1 1. Tools Dynamic Display 2. STK Dynamic Display Tool Styles Classical Orbital Elements Open Dynamic Display 3. Dynamic Display 4. Dynamic Display STK Dynamic Display : 117
118 STK 2 STK 118
119 STK 2 GraphScen 1. GraphScen 2. Basic Properties 3. Time Period Start Time Stop Time Epoch 1 Nov :00: Nov :00: Nov :00:
120 STK 2 GraphScen 4. Animation Start Time Stop Time Time Step Refresh Delta 1 Nov :00: Nov :00: seconds Change to High Speed 5. Units Distance Unit Time Unit Date Format Angle Unit Mass Unit Kilometers Seconds Gregorian UTC Degrees Kilograms 120
121 STK 2 GraphScen Orbit Wizard MEO 8. MEO Basic Properties Orbit Propagator Period Eccentricity Inclination Lon of Ascending Node True Anomaly J4 Perturbation seconds
122 STK 2 GraphScen Vandenberg AfricaFac 11. Basic Properties Position Geodetic Vandenberg AfricaFac Latitude Longitude Altitude Latitude Longitude Altitude km 122
123 STK 2 1. MEO Tools Graph STK Graph Tool Styles Solar AER Create MEO Solar AER / / 123
124 STK 2 2. Graph X Y 3. Graph Files Units Use Default Report Units Angle Unit Radians 4. Graph Edit Attributes 5. Graph 124
125 STK 2 1. MEO STK Graph Tool New Style NewStyle CartZ Change 2. CartZ Properties TimeXy Graph Type Cartesian Position Fixed z y Axis y Axis Cartesian Fixed Z 3. Create xy 4. Restore STK Graph Tool 125
126 STK 2 5. STK Graph Tool Styles CartZ Properties Layout Title Time/CartZ Graph Layout Options Tick Grid 6. STK Graph Tool Create 126
127 STK 2 7. Graph Style Properties Content Cartesian Position Fixed Shift x y y Axis y Axis Title Cartesian Fixed X-Y-Z Create
128 STK 2 1. MEO Tools Access 2. Access Associated Objects AfricaFac Compute Vandenberg Compute Access Graphs Access 128
129 STK 2 6. Access Remove All 129
130 STK 2 1. MEO, Tools Strip Chart 2. STK Strip Chart Tool Styles Classical Orbital Elements Open
131 STK 3 STK 131
132 STK 3 AccessScen 1. AccessScen 2. Basic Properties 3. Time Period Start Time Stop Time Epoch 1 Nov :00: Nov :00: Nov :00:
133 STK 3 AccessScen 4. Animation Start Time Stop Time Time Step Refresh Delta 1 Nov :00: Nov :00: seconds Change to High Speed 5. Units Distance Unit Time Unit Date Format Angle Unit Mass Unit Kilometers Seconds Gregorian UTC Degrees Kilograms 133
134 STK 3 AccessScen Orbit Wizard LEO MEO 8. Basic Properties Orbit LEO MEO Propagator Period Eccentricity Inclination Propagator Mean Motion Eccentricity Inclination Long Of Ascending Node J4 Perturbation 9000 seconds TwoBody 5 revs per day
135 STK 3 AccessScen 9. Colorado_Springs Perth 10. Basic Properties Geodetic Colorado_Springs Perth Latitude Longitude Altitude Latitude Longitude Altitude km : 135
136 STK 3 AccessScen 11. Colorado_Springs FacSensor LEO SatSensor 12. Basic Properties Definition Simple Conic Cone Angle
137 STK 3-1. SatSensor Tools Access 2. Associated Objects Colorado_Springs Compute Static Highlight * Colorado_Springs 137
138 STK Access Reports Access Access SatSensor Colorado_Springs 5. Access Remove Access 6. SatSensor Perth 7. Access 138
139 STK 3-1. FacSensor Graphics Properties Projection Maximum Altitude 1000km Step Count 1 2. FacSensor Access LEO Compute SatSensor Colorado_Springs 3. Access MEO Compute Access MEO Reports Access FacSensor MEO Access Remove All 139
140 STK 3-1. SatSensor Access MEO SatSensor MEO SatSensor MEO SatSensor MEO 2 4. Access Remove All Access 140
141 STK 3 1. SatSensor Basic Properties Pointing Pointing Type Targeted Available Targets Perth Assigned Targets 2. LEO LEO Perth 3. SatSensor Basic Pointing Assigned Targets Perth Pointing Fixed 4. FacSensor SatSensor Basic Graphic Half-angle Maximum Altitudes Step Counts Pointing : 141
142 STK 3 1. FacSensor Access LEO Access 2. FacSensor Properties Constraints Constraints Properties 3. Basic MaxAximuth Angle Colorado_Springs 5. Constraints Properties Max Azimuth Angle Max Elevation Angle Max Elevation Angle Min Max Range Min 4000km Max 6000km 142
143 STK AccessScen Tools Remove Accesses 143
144 STK 3 1. SatSensor Access Perth Access 2. Perth Properties Constraints 3. Sun Max Sun Elecation Angle
145 STK Max Sun Elevation Angle 6. SatSensor Constraints Properties 7. Sun Min Sun Elevation Angle Min Sun Elevation Angle Lighting Umbra Constraints Properties 10. AccessScen Tools Remove Accesses 145
146 STK 4 STK Walker Walker Walker ( ) Walker ( ) 146
147 147 STK 4 Walker Walker Walker t =s p f f 360 /t f 0 p-1 STK Walker Tools Walker Walker RAAN 2 90 RAAN 180 RAAN 360
148 STK 4 Walker Walker 1. Walker 2. Basic Properties 3. Time Period Start Time Stop Time Epoch 1 Jan :00: Jan :00: Jan :00:
149 STK 4 Walker Walker 4. Animation Start Time Stop Time Time Step Refresh Delta 1 Jan :00: Jan :00: seconds Change to High Speed 5. Units Distance Unit Time Unit Date Format Angle Unit Mass Unit Kilometers Minutes Gregorian UTC Degrees Kilograms 149
150 STK 4 Walker 1. WhiteSands 2. WhiteSands Basic Properties Type Latitude Longitude Altitude Geodetic km 3. Facsensor 4. Basic Properties Definition Sensor Type Cone Angle Simple Conic Graphic Properties Projection Max Altitude km Step Count 1 150
151 STK 4 Walker 6. W Basic Properties Semimajor Axis Period Propagator Period Eccentricity Inclination Argument of Perigee RAAN True Anomaly Two Body 120 min W Graphic Properties Pass Leading/Trailing Ground Track Lead Type One Pass 8. fov 151
152 STK 4 Walker 9. Basic Properties Definition Sensor Type Cone Angle Simple Conic
153 STK 4 Walker Walker 1. W Tools Walker Walker Number of Planes 3 Number of Sats per Plane 4 Inter-plane Spacing n 2 n Walker Number of Planes 2 Number of Sats per Plane 4 Inter-plane Spacing 1 153
154 STK 4 Walker Walker
155 STK 4 Walker Walker 1. Walker 2. Tools Report Report Tool Style Lighting Times Report Tool Style Classical Orbit Elements Time Period 5. Time Period Stop Time 1 Jan :01:00.00 Change 1 Jan :00:00 1 Jan :01: Report Tool Create 155
156 STK 4 Walker Walker 7. RAAN True Anomaly 8. Report Tool 9. Tools Graph Styles Lighting Times Create 10. Graph Attributes 11. Graph Tool 156
157 STK 4 Walker 1. Walker 2. Report Tool New TrueAnomRAAN Change 3. TrueAnomRAAN Properties 4. Content Classical Elements -J2000 Time RAAN True Anomaly Ctrl Report Contents Report Tool Time Period Stop Time 1 Jan :01: Report Tool TrueAnomRAAN 8. Report Tool 157
158 STK 4 Walker 1. Walker 2. Graph Tool New TrueAnomRAAN Change 3. TrueAnomRAAN Properties 4. Content Graph Type TimeXY Classical Elements -J2000 Time RAAN True Anomaly Ctrl Y Axis 5. Graph Tool Create TrueAnomRAAN 6. Attributes
159 STK 4 Walker 1. Tools Access Access Walker Compute 2. Report Access 3. Access
160 STK 4 Walker Walker 2 Chain Constellation 1. Constellation WalkerCon 2. Basic Properties Constellation Objects 3. Constraint Properties Restriction Any of 4. Chain WhiteSandWalkerCon Basic Properties WhiteSands WalkerCon 5. Report Complete Chain Access 160
161 STK 4 Walker Walker Individual Stand Access 8. Access Report Tool 9. Graphic Properties Show Static Animation 10. Tools Graph Graph Tool Complete Chain Access 11. Individual Strand Access
162 Satellite Tool Kit STK 162
163 Satellite Tool Kit STK Lifetime LOP 163
164 STK STK 164
165 STK 1 STK
166 STK 1 STK 3 / 166
167 STK 1 AAM 1. AAM 2. Basic Properties 3. Time Period Start Time Stop Time Epoch 1 Jan :00: Jan :00: Jan :00:
168 STK 1 AAM 4. Animation Start Time Stop Time Time Step Refresh Delta 1 Jan :00: Jan :00: seconds Change to High Speed 5. Units Distance Unit Time Unit Date Format Angle Unit Mass Unit Kilometers Seconds Gregorian UTC Degrees Kilograms 168
169 STK 1 AAM 6. AAmSat 7. Basic Basic Properties Orbit Step Size Propagator Coord. Type Coord. System Radius Azimuth Declination RAAN 60 seconds Two Body Spherical J km 61.5º 0º 0º
170 STK 1 1. AAM Tools City Database 2. City Database City Name Lis* Country Portugal 3. Perform Search 4. Search Results Lisboa Facility Creation 170
171 STK 1 5. Cancel City Database Search Results Lisbon 6. AAM Facility Database 7. Facility Database Site Name C* Perform Search City Database Search Results Canberra26 8. Facility Database 9. AAM Tools Star Database 10. Star Database Common Name Sirius Perform Search Star Database Search Results
172 STK Star Database 12. Reset HR
173 STK 1 1. Area Target NWATarget 2. Basic Properties 3. Boundary Insert Point Latitude 31.0º 19.8º 19.9º 30.3º Longitude -8.2º -7.8º 5.6º 5.6º Animate Forward AAmSat Reset 173
174 STK 1 1. AAmSat 2 DownSens UpSens 2. DownSens Basic Basic Properties Definition Sensor Type( Rectangular Vertical Horizontal Half Angles 45º 3. Pointing Pointing Type Fixed 4. 2 UpSens Basic Properties Definition Complex Conic Sensor Type Outer Half Angle 10º Maximum Clock Agnle 360º 5. Pointing Targeted Pointing Type Tracking Boresight Type Rotate About Boresight 174
175 STK 1 6. Available Targets Star/Hr-2491, Assigned Targets 7. Reset 175
176 STK 1 8. UpSens Tools Access Access Associated Objects HR-2491 Compute 9. Reset 10. Access Remove Access 11. Lisboa Tools Access Access Associated Objects AAmSat Compute 12. Reset 13. Access Remove Access 176
177 STK DownSens Tools Access Access Associated Objects NWATarget Compute Access 15. Associated Objects Canberra26 Compute 16. AAmSat NWATarget NWATarget Canberra Reset 18. Access 177
178 STK 1 1. DownSens Properties Constraints 2. Temporal Local Start End Min Max Duration 3. Duration Min 0 Max 700 sec DownSens NWATarget 4. Max Duration Local Min Max 178
179 STK 1 5. DownSens Constraints Properties Zones Exclusion Zone Add 6. Exclusion Zone Latitude Longitude Min Max Min Max -40º -20º 130º 150º Exclusion Zone Delete Constraints Properties 9. Tools Remove Accesses 179
180 STK STK HPOP 180
181 STK 2 STK HPOP 181
182 STK 2 DragParadox 1. DragParadox 2. Basic Properties 3. Time Period Start Time Stop Time Epoch 1 Jan :00: Jan :00: Jan :00:
183 STK 2 DragParadox 4. Animation Start Time Stop Time Time Step Refresh Delta 1 Jan :00: Jan :00: seconds Change to High Speed 5. Units Distance Unit Time Unit Date Format Angle Unit Mass Unit Kilometers Minutes Gregorian UTC Degrees Kilograms 183
184 STK 2 DragParadox File Save As DragParadox.sc 184
185 STK 2 HPOP 1. Satellite HPOP1 HPOP1 Basic Properties Orbit HPOP Propagator 2. Semimajor Axis Period Period 95 min 3. Force Models HPOP Force Model Earth Gravity Third Body Gravity Drag Gravity Field - JGM2.gv Maximum Degree - 21 Maximum Order 21 Use Solar Gravity - ON Use Lunar Gravity - ON Use - ON Cd Atm Density Model - Harris-Priester 185
186 STK 2 HPOP Drag Solar Radiation Pressure Average F Area/Mass Ratio m 2 /kg Use - ON Cp Area/Mass Ratio m 2 /kg 4. HPOP Force Model Basic Properties 5. HPOP1 Graphics Properties Marker Style Star HPOP2 Force Models Drag HPOP1 Graphics Properties Marker Style Circle
187 STK 2 HPOP 8. HPOP2 HPOP1 HPOP1 HPOP2 187
188 STK 2 HPOP1 HPOP2 LEO 4 HPOP1 188
189 STK 2 = - /2a = = a= 189
190 STK 2 1. Tools Report Classical Oribt Elements 2. LLA Position 3. Tools Graph STK Graph Tool New Altitude Change 4. Altitude Properties Content TimeXY Graph Type LLA State Fixed Alt Y-Axis STK Graph Tool Create 5. Edit Attributes STK Graph Tool 190
191 STK 2 6. Strip Chart 7. STK Strip Chart Tool Styles Altitude Open 8. HPOP1 Altitude HPOP2 HPOP1 HPOP1 HPOP2 HPOP
192 STK 2 1. HPOP2 Edit Copy Edit Paste HPOP2 TwoBody Basic Properties Propagator TwoBody TwoBody Graphics HPOP2 2. TwoBody HPOP2 TwoBody 3. HPOP2 TwoBody Tool Graph STK Graph Tool Radius Graph Style Properties Content TimeXY Graph Type LLR Fixed Rad Y-Axis STK Graph Tool Create 4. Edit Attributes 192
193 STK 2 5. STK Graph Tool Altitude Create º HPOP HPOP2 TwoBody Radius TwoBody 193
194 STK 2 7. TwoBody Altitude 194
195 STK 2 1. Graphics Properties Global Attributes Show Ground Tracks 2. Tool New Map Window 3. Map Properties Details Show Lat/Lon Lines Projection Projection Type Perspective Projection Alt Center 11500km 4. Reset 5. Projection Alt 10000km Lat 8º Lon 37º 195
196 STK Center Altitudes 8. Map Properties
197 STK STK LOP LOP 197
198 STK 3 LOP LOP LOP LOP LOP 1976 LOP J21 LOP NASA JPL 198
199 STK 3 LOP LOP 1. LOP 2. Basic Properties 3. Time Period Start Time Stop Time Epoch 1 Jan :00: Jan :00: Jan :00:
200 STK 3 LOP LOP 4. Animation Start Time Stop Time Time Step Refresh Delta 1 Jan :00: Jan :00: seconds Change to High Speed 5. Units Distance Unit Time Unit Date Format Angle Unit Mass Unit Kilometers Seconds Gregorian UTC Degrees Kilograms 200
201 STK 3 LOP Satellite SatLOP1 3. SatLOP1 Basic Properties Orbit Start Stop Time Step Size LOP 1 Propagator Step Size Period Eccentricity Inclination LOP 1 day 5700 seconds 0.0º 35.0º 201
202 STK 3 LOP 4. Force Models 202
203 STK 3 LOP 5. LOP Force Models Earth Gravity Third Body Gravity Drag Solar Radiation Pressure Gravity Field JGM2.gv Maximum Degree 12 Maximum Order - 12 Use Solar Gravity ON Use Lunar Gravity - ON Use ON Cd - 3 Use ON Cp 1.5 Atmosphere 90 km Physical Data Drag Cross-Sectional Area 25.0 m 2 SRP Cross-Sectional Area 25.0 m 2 Satellite Mass kg 203
204 STK 3 LOP 6. SatLOP2 SatLOP2 Basic Properties Orbit Start Stop Time Step Size LOP 1 Propagator Step Size Period Eccentricity Inclination LOP 1 day 5700 seconds 0.0º 35.0º 7. Force Models 204
205 STK 3 LOP Drag Solar Radiation Pressure Use Off Use ON Cp 1.5 Atmosphere 90 km Physical Data Drag Cross-Sectional Area N/A SRP Cross-Sectional Area 25.0 m 2 Satellite Mass kg 205
206 STK 3 LOP X Y Z 1. SatLOP1 Shift SatLOP1 SatLOP2 Tools Dynamic Display 2. Dynamic Display Tool ECF Position Velocity Open SatLOP1 SatLOP Jan Jan SatLOP1 SatLOP2 4. Dynamic Display Tool 206
207 STK 3 LOP 1. SatLOP1 Tools Graph 2. Graph Tool LLA Position Time Period Stop Time 10 Jan :00:00 Change 3. SatLOP2 4. Graph Tool 5. SatLOP1 SatLOP2 Basic Properties Force Model
208 STK STK Lifetime 208
209 STK 4 Lifetime NASA 1970 Jacchia Lifetime J5 Lifetime Lifetime 209
210 STK 4 Lifetime Lifetime Lifetime 210
211 STK 4 LIF 1. LIF 2. Basic Properties 3. Time Period Start Time Stop Time Epoch 1 Jan :00: Jan :00: Jan :00:
212 STK 4 LIF 4. Animation Start Time Stop Time Time Step Refresh Delta 1 Jan :00: Jan :00: seconds Change to High Speed 5. Units Distance Unit Time Unit Date Format Angle Unit Mass Unit Kilometers Seconds Gregorian UTC Degrees Kilograms 212
213 STK 4 LIF 6. 3 TwoBody J4SAT HPOP 7. TwoBody J4SAT Basic Properties Orbit 60 TwoBody J4SAT Propagator Apogee Altitude Perigee Altitude Inclination Propagator Apogee Altitude Perigee Altitude Inclination TwoBody 700km 700km 35.0º J4Perturbation 800km 800km 55.0º 213
214 STK 4 HPOP 1. HPOP Basic Properties Orbit 60 Propagator HPOP Period 5900 sec Inclination 35.0º 2. Orbit Force Models 214
215 STK 4 HPOP 1. HPOP Force Model Earth Gravity Third Body Gravity Drag Solar Radiation Pressure Gravity Field JGM2.gv Maximum Degree 21 Maximum Order - 21 Use Solar Gravity ON Use Lunar Gravity - ON Use ON Cd 2.0 Atm Density Model Harris-Peiester Average F Area/Mass Ratio m 2 /kg Use ON Cp 2.0 Area/Mass Ratio 100.0m 2 /kg 215
216 STK 4 1. HPOP Tools Lifetime 2. Lifetime Drag Coefficient 2.0 Reflection Coefficient Drag Area m 2 Area Exposed to SUN 1000 m 2 Mass 1000 kg 216
217 STK 4 3. Graphics Compute Information 4. Lifetime HPOP 217
218 STK 4 1. HPOP TwoBody TwoBody Tools Lifetime 2. Lifetime HPOP 3. Lifetime 4. HPOP Basic Properties Orbit Apogee Altitude Perigee Altitude Tools Lifetime 6. Lifetime 218
219 STK 4 1. J4SAT Lifetime Drag Area Area Exposed to Sun m 2 Comoute 2. Information Lifetime Drag Area Area Exposed to Sun 3. Lifetime Drag Area Area Exposed to Sun 1000m 2 Advanced 219
220 STK 4 4. Lifetime Advanced Orbit per Calculation 100 Lifetime Compute Orbit per Calculation 5. Lifetime Advanced 2nd Order Oblateness Correction Lifetime Advanced Rotating Atmosphere Rotating Atmosphere 6. Lifetime
221 STK STK Az-El - VO 221
222 STK º / STK 222
223 STK 5 Terrain 1. Terrain 2. Basic Properties 3. Time Period Start Time Stop Time Epoch 1 Jan :00: Jan :00: Jan :00:
224 STK 5 Terrain 4. Animation Start Time Stop Time Time Step Refresh Delta 1 Jan :00: Jan :00: seconds Change to High Speed 5. Units Distance Unit Time Unit Date Format Angle Unit Mass Unit Kilometers Seconds Gregorian UTC Degrees Kilograms 224
225 STK 5 Terrain 6. Terrain Add Terrain Source Selection Type AGI World Terrain 7. Location a. PC X:\terrain\world30.hdr X b. UNIX /CDROM/terrain/world30.hdr
226 STK 5 1. VO VO 2:1 2. Details Coastlines 3. Resolution Use Very Low to Super High 226
227 STK 5 4. Very Low km/pixel / High Very High 5. Resolution Very High to Super High 3 km 227
228 STK 5 6. Resolution Use Use 7. Resolution Very Low to Low Low to Medium Medium to High High to Very High Very High to Super High 20 km 10 km 5 km 1 km 0.1 km
229 STK 5 1. Tsat 2. Tsat Basic Properties Orbit J4 Perturbation 3. Semimajor Axis Apogee Altitude Perigee Altitude Apogee Perigee Altitudes 300km Inclination 45º Longitude of the Ascending Node 240º 4. City Database City Name Denver* Province/State / Col* Perform Search City Database Search Results Denver Creation Class Facility 229
230 STK 5 5. Denver Basic Properties Use Terrain Information AzElMask Use Terrain Data Height Adjustment 0.0km Basic Properties 6. STK/VO Denver VO Properties Model Scale
231 STK 5 AzEl / 1. Denver Graphic Properties AzElMask Show Mask 1.615km 50km VO 4. Denver Report Azimuth Elevation 5. Basic Properties AzElMask Use Terrain Information 6. Report Tool 231
232 STK 5 VO VO Globe File Editor 1. Tools Globe File Editor 2. Globe File Editor Globe File AGI 1024 LOD 0 Globe Texture AGI 1024 Add Terrain Data 3. Add Terrain Data Terrain Data Terrain Region CD 4. Location North West East South
233 STK 5 VO 5. Terrain Color Min Red Green 100 Blue Terrain Scale Globe File Editor Terrain Region-World30 Globe Texture 8. Globe File Editor Save As Terrainex 9. Globe File Editor 233
234 STK 5 VO 1. AVO VO Globe Surface Terrainex.glb 2. Texture Smooth 3. AVO Facility/Denver Use as Position and Direction 4. VO
235 STK 5 1. Globe File Editor 2. Edit Selected 3. Terrain Color Min Red Green0.0 Blue 255 Scale Factor Globe File Editor Save 5. AVO
236 Satellite Tool Kit STK 236
237 Satellite Tool Kit STK 237
238 STK 1 STK 238
239 STK 1 STK / STK STK
240 STK 1 Chains 1. Chains 2. Basic Properties 3. Time Period Start Time Stop Time Epoch 1 Jan :00: Jan :00: Jan :00:
241 STK 1 Chains 4. Animation Start Time Stop Time Time Step Refresh Delta 1 Jan :00: Jan :00: seconds Change to High Speed 5. Units Distance Unit Time Unit Date Format Angle Unit Mass Unit Kilometers Seconds Gregorian UTC Degrees Kilograms 241
242 STK 1 Chains 6. LEO 2 MEO 7. LEO Basic Properties Orbit Start Time Stop Time Step Size Propagator Orbit Epoch Apogee Altitude Perigee Altitude Inclination Lon of Ascending Node 1 jan :00: jan :00: seconds J4 perturbation 1 jan :00: km 600 km
243 STK 1 Chains 8. MEO Basic Properties Orbit Start Time Stop Time Step Size Propagator Orbit Epoch Mean Motion Eccentricity Inclination Lon of Ascending Node 1 jan :00: jan :00: seconds J4 perturbation 1 jan :00: revs per day SC DC Basic Properties Geodetic 243
244 STK 1 Chains SC DC Latitude Longitude Altitude Latitude Longitude Altitude km km 10. DC Shift SC Graphics 11. Graphics Properties Marker Type 244
245 STK 1 Chains 245
246 STK 1 1. Chains SC_LEO_MEO_DC 2. Basic Properties Definition Available Objects SC Chain Objects 3. LEO MEO DC Chain Objects Chain Objects 4. SC_LEO_MEO_DC Tools Report STK Report Tool Styles Complete Chain Access Create 5. Individual Object Access Time Ordered Access STK Report Tool 246
247 STK 1 1. Constellation Satellites 2. Satellites Basic Properties Constellation Available Objects LEO Shift MEO Constellation Objects 3. Satellites Constraint Properties Any of( 4. SC_Satellites_DC Basic Properties Definition SC Satellites DC Chain Objects 247
248 STK 1 5. SC_Satellites_DC Tool Report STK Report Tool Complete Chain Access Create 6. Individual Strand Access Time Ordered Access 7. 3 STK Report Tool 8. SC_Satellites_DC STK Graph Tool Individual Object Access 248
249 STK STK Graph Tool Individual Strand Graph 11. STK Graph Tool 249
250 STK NoSat NoSat Basic Properties Constellation MEO LEO Any Of Exactly N N 0 Exactly 0 2. Chains 1 SC_NoSat_DC Basic Properties Definition SC NoSat DC 3. SC_NoSat_DC Tools Report Complete Chain Access 250
251 STK 1 4. STK Report Tool 5. SC_NoSat_DC Tools Graph Cmplete Chain Access X Y 6. SC_Satellites_DC Complete Chain Access STK Graph Tool 251
252 STK 1 1. SC_Satellites_DC Report Complete Chain Access 2. LEO Properties Constraints Azimuth Angle Maximum Angle 180º 3. Files Refresh 4. Constraints Properties Azimuth Constraint 5. DC Constraints Properties Basic Maximum Range 12000km Maximum Elevation Angle 70º 252
253 STK 1 6. Files Refresh 7. Constraints Properties
254 STK 2 STK Walker 254
255 255 STK 2 STK / / 1 LEO 3% 50 1 GEO 42% 3 GEO GEO MEO 1 MEO 31% 12 MEO MEO GEO MEO STK Training Exercises Chains
256 STK Foursats 2. Basic Properties Definition 4 3. Properties Constraints Basic Any Of 4. ChainFourSats 5. Basic Properties Available Objects Colordo_Springs Foursats 256
257 STK 2 6. Tools Report STK Report Tool Complete Chain Access 7. Individual Strand Access STK Report Tool 8. Graph 9. STK Graph Tool Number of Accesses 10. STK Graph Tool 257
258 STK 2 1 Walker 12 MEO 1 3 Walker STK Walker 1. ChainFourSats relay1 FourSats comsat2 comsat3 comsat4 comsat1 Edit Cut File Remove 2. comsat1 Tools Walker Walker Walker Delta Planes 3 satellites per plane 4 Interplane Spacing 1 RAAN Spread 360º comsat1 258
259 STK 2 1 Walker 4. colorado_springs Basic Properties Pointing 12 Assigned Targets 5. relay Walker comm_net Basic Properties 12 comsat1 7. Constraints Properites Basic Any Of 8. 1 comchain relay1 comm_net 9. Complete Chain Access
260 STK 2 1 Walker 10. Constellation Constraints At Least N File Refresh 12. Constellation Constraints Exactly N File Refresh 14. STK Report Tool 15. Constellation Constraints Any Of 260
261 STK 2 1. agi300 mobilink Basic Properties Pointing Pointing Type Targeted comchain Graphics Properties Show Static Graphics Show Line Show Highlight
262 STK 2 12 MEO (Crosslinking - 262
263 STK 2 1. agi500 crosslink Basic Properties Pointing Pointing Type Targeted crosslink 3. comchain Report Tool Complete Chain Access 4. STK Report Tool 263
264 STK 2 Colorado_Springs 3 1. STK Details Background Image BlackNeon 2. Tools Remove Accesses 3. relay1 Access Show Line Animate Highlight Static Highlight Access 4. Colorado_Springs 5. crosslink 264
265 STK 2 6. STK 20 agi crosslink Access 9. agi
266 STK Colorado agi500 Colorado_springs agi Tools Remove Accesses 13. crosslinking comsat comsat comsat111 Access * Access
267 STK comchain relay1 comm_net agi500 crosslink 17. Angle Between 18. STK Report Tool 267
268 STK Walker 12 1 Shift 1 File Remove comsat1 3 5 Walker 3. relay1 Basic Properties Pointing 15 Assigned Targets 4. comm_net 15 relay1 agi500 comm_net 5. Complete Chain Access 268
269 STK Tools Remove Accesses 269
270 STK STK Connect 1 270
271 STK STK STK Connect STK - Connect STK Connect IPC STK UNIX TCP/IP Connect STK Connect STK Connect STK Connect 271
272 STK STK Connect Connect Connect 1. Windows MSDOS agi/stk/4.2.1/connect/bin/intelrelease agipcexp.exe UNIX telnet localhost Connect ipccontrol / ackon 1 STK ACK NACK ACK NACK 272
273 STK STK Connect 3. Connect Con_ex 1 Jan Jan 2001 Epoch Time 1 Jan 2001 New / Scenario Con_ex SetTimePeriod Scenario/Con_ex 1 Jan :00:00 2 Jan :00:00 SetEpoch Scenario/Con_ex 1 Jan :00: New / Scenario/*/Satellite ISS Set StateCart */Satellite/ISS J4Perturbation 1 Jan :00: Jan :00: J Jan :00: * / scenario/scenario_name 273
274 STK STK Connect º 360º New /*/Satellite/ISS/Sensor sensorman Define Scenario/Con_ex/Satellite/ISS/Scensor/sensorman Conical EC New / Scenario/Con_ex/Facility/EC Set Position Scenario/Con_ex/Facility/EC EC point Scenario/Con_ex/Satellite/ISS/Sensor/sensorman TargetTrack Facility/EC 274
275 STK STK Connect 8. 1 KSC New /Scenario/Con_ex/Facility ksc Setpoition Scenario/Con_ex/Facility/ksc KSC Addassignedtarget Scenario/Con_ex/Satellite/ISS/Sensor/sensorman Facility/ksc 10. Animate Scenario/* SetValues 1 Jan :00: Animate Scenario/* start Ipccontrol / ackoff 275
276 STK/VO VO STK VO VO VO VO View Pilot VO VO View Path Editor 276
277 STK/VO VO STK VO STK/VO View Pilot View Path Editor VO VO View Pilot View Path Editor 277
278 STK/VO VO VOTool 1. VOTool 2. Basic Properties 3. Time Period Start Time Stop Time Epoch 1 Jan :00: Jan :00: Jan :00:
279 STK/VO VO VOTool 4. Animation Start Time Stop Time Time Step Refresh Delta 1 Jan :00: Jan :00: seconds Change to High Speed 5. Units Distance Unit Time Unit Date Format Angle Unit Mass Unit Kilometers Seconds Gregorian UTC Degrees Kilograms 279
280 STK/VO VO 1. 1 LEO Basic Orbit Semimajor Axis Period RAAN Lon. Ascn. Node Start Time Stop Time Step Size 1 an :00: Jan :00: seconds Propagator Period Inclination Lon of Ascending Node TwoBody 6600 sec
281 STK/VO VO 3. 1 DC 4. Basic Properties Position Geodetic Latitude Longitude Altitude 39.0º -77.0º 0.0 km LEO 1 LEO 1 LEO Look Basic Properties Simple Conic Cone Angle 15.0º 7. VO Reset Animate Forward VO Reset 281
282 STK/VO VO VO 1. VO Graphics Properties 2. Globe Surface Show option Texture ON Advanced.glb Show ON Smooth OFF Central Body Earth Show Clouds OFF 3. Celestial Show Sun Show Sun Label Show Moon Show Moon Label Show Stars Grids Celestial Grid 4. Annotation Show Time Viewer Position 282
283 STK/VO VO VO VO Tools VO Toolbar Options 7. Toolbar Options OFF Animation Mode VO X Mouse Speed Controls 8. VO
284 VO 2. VO STK/VO VO Shift+ ctrl+ VO HomeView VO VO PC UNIX Shift+ ctrl+
285 STK/VO VO VO 3. Shift VO 4. VO VO 285
286 STK/VO VO View Pilot VO HomeView ECI View Pilot VO 1 Viewer Position Viewer Direction Viewer Position 1. VO Graphics Properties Grids Show Grid Celestial Show Stars 2. VO View Pilot 286
287 STK/VO VO View Pilot 3. Viewer Position Satellite/LEO Direction Satellite/LEO 1 Stored Views LEO New LEO Stored View 287
288 STK/VO VO View Pilot 4. Viewer Position Satellite/LEO Direction Satellite/LEO 1 Stored Views LEO New LEO Stored View 5. ECI 6. DC DC Position Direction DC Position Direction VO Viewer Direction 288
289 STK/VO VO View Pilot 7. Stored Views Position Direction Modify 8. VO Position/Direction View Position LEO Use as Position and Direction 9. VO View 10. Use as Position and Direciton 11. HomeView 289
290 STK/VO VO VO 1. LEO VO 2. VO Properties Vector Show Sun VVLH Moon Sun Persistence Duration 600 Transparent 3. Model 290
291 STK/VO VO VO 4. Show Model Model Scale 3.0 VO Use Levels 5. Model Models File Model File Select File Hubble.mdl VO View Position LEO Use as Position and Direction 8. VO LEO VO Hubble Sun 291
292 STK/VO VO VO 9. Model Articulations View 10. Articulation LOD 0 VO Articulations SSARt Transformation yleftrot VO 292
293 STK/VO VO VO 12. Articulation 0, 13. Model 293
294 STK/VO VO VO 1. VO Properties Attributes Show Pulses Translucency 60% 2. Pulse Show Pulse Amplitude Wavelength Frequency Style Smooth ON Sine OFF
295 STK/VO VO VO 4. VO View Up 5. View Position and Direction LEO 6. Pulse Amplitude 1,Wavelength 200,Frequency VO Properties Attributes Show Pulses 295
296 STK/AVO VO STK/AVO STK/AVO STK/AVO STK/AVO Soft VTR STK/AVO VO 3 296
297 STK/AVO VO 1. VOTools Basic Properties Animation Time Step 10 min 2. Tools VO Toolbar Options VO Toolbar Options Viewpath Control 3. VO View Path Editor 297
298 STK/AVO VO 4. Name Earth-Fly-By New 5. VO HomeView HomeView ECI VO 6. VO Step Forward VO 10: ~20 7. VO Reset 298
299 STK/AVO VO 8. View Path Editor Add 9. VO Add ~20 Add View Viewer Position Driection LEO ~10 299
300 STK/AVO VO 15. View Path Editor Show Path Color Red 16. VO Homeview 300
301 STK/AVO VO 17. View Path Editor Show Up/Look Vectors VO Reset 19. Decrease Time Step 1 VO Step Forward 20. Reset 21. View Path Editor Show Up/Look Vectors Show Path Follow Path While Animating 301
302 STK/AVO VO
303 STK/AVO 3D 3D VO MDE 3D 3D 303
304 STK/AVO 3D 3D STK/VO STK MDE VO 3D 3D 3D ASCII.mdl STK 3D 304
305 STK/AVO 3D 3D Vehicle.mdl Vehicle Refer Refer Refer Body SolarPanel SolarPanel Cylinder Polygon 305
306 STK/AVO 3D Basicmod 1. Basicmod 2. Basicmod Properties Basic 3. Time Period Start Time Stop Time Epoch 1 Jan :00: Jan :00: Jan :00: Animation Start Time Stop Time Time Step Refresh Delta 1 Jan :00: Jan :00: sec High Speed 306
307 STK/AVO 3D Basicmod 5. Unit Distance Unit Time Unit Date Format Angle Unit Mass Unit Kilometers Seconds Gregorian UTC Degrees Kilograms
308 STK/AVO 3D 1. Orbit Wizard BasMod 2. BasMod Basic 3. Orbit Semimajor Axis Apogee Altitude Start Time Stop Time Step Size Propagator Apogee Altitude Perigee Altitude Inclination RAAN True Anomaly 1 Jan :00: Jan :00: sec TwoBody 300km 300km
309 STK/AVO 3D MDE Model Development Environment MDE 1. MDE Satellite Tool Kit4.x Modeler 2. PC WordPad UNIX VI 3. 1NewModel.mdl STKData/VO/Model MDE 309
310 STK/AVO 3D MDE extrusion, cylinder, helix, polygon, polygonmesh, revolve, skin sphere MDE Refer root 310
311 STK/AVO 3D 1. extrusion 2. Orange 10 4 Component MainBody Extrusion FaceColor orange Length 10 NumVerts 4 Data EndExtrusion EndComponent 3. MDE Root 311
312 STK/AVO 3D 1. Component Body Refer Component MainBody EndRefer EndComponent Component NewMod Root Refer Component Body EndRefer EndComponent 2. 1NewModel 3. MDE File Open Model 1NewModel
313 STK/AVO 3D 5. MDE View Show Axes PC XYZ extrusion 313
314 STK/AVO 3D 2 1. polygons MainBody 314
315 STK/AVO 3D Component MainTop1 Polygon Translate FaceColor purple NumVerts 4 Data EndPolygon EndComponent Component MainTop2 Polygon Translate FaceColor white NumVerts 4 Data EndPolygon EndComponent 315
316 STK/AVO 3D 1. Component MainTop Refer Component MainTop1 EndRefer Refer Component MainTop2 EndRefer EndComponent 2. Component MainBottom Polygon FaceColor green Translucency 0.5 NumVerts 4 Data EndPolygon EndComponent 316
317 STK/AVO 3D 1. Refer MainBody EndRefer MDE File Open Model 1NewModel 4. translucency Refer Component MainTop EndRefer Refer Component MainBottom EndRefer 317
318 STK/AVO 3D 1. MainBottom 2. translation XYZ Component HelixTop Helix Translate FaceColor grey80 NumSides 20 NumCoils 15 CoilHeight 5.0 CoilRadius 1.5 WireRadius 1.0 EndHelix EndComponent 3. Helix 318
319 STK/AVO 3D Component Ring Cylinder Translate Rotate FaceColor blue NumSides 16 Face1Position Face1Radius 3.5 Face1Normal Face2Position Face2Radius 3.5 Face2Normal EndCylinder EndComponent 1. Refer Refer Component HelixTop EndRefer Refer Component Ring EndRefer 319
320 STK/AVO 3D MDE
321 STK/AVO 3D 1. door Cylinder Component BottomDoor Polygon FaceColor DarkSeaGreen NumVerts 4 Data EndPolygon EndComponent 321
322 STK/AVO 3D 2. BottomDoor 3. Door Z 0 90 DoorOpen Component DoorOpen Refer Component BottomDoor EndRefer Articulation DoorOpen zrotate ZRotate EndArticulation EndComponent 4. Refer Refer Refer Component DoorOpen EndRefer 322
323 STK/AVO 3D 5. MDE Door 6. MDE Edit Articulations Articulations, DoorOpen 7. DoorOpen Transformations ZRotate 0~90 8. ZRotate Door 9. Scale
324 STK/AVO 3D Component BigRing Refer Component Ring EndRefer Articulation ScaleRing xscale ScaleX yscale ScaleY EndArticulation EndComponent 1. Ring 1~5 2. Refer Ring BigRing 3. Refer Component BigRing EndRefer 4. MDE 324
325 STK/AVO 3D 5. Ring 1~5 6. Edit Articulations ScaleRing 7. ScaleRing Transformation ScaleX ScaleY ScaleX Ring 8. ScaleY 9. X Y 1 Articulation 10. MDE VO 325
326 STK/AVO 3D VO VO 1. STK VO 2. Model 3. 1NewModel.mdl VO Apply 4. VO View Position and Direction Satellite/BasMod View as Position & Direction 5. VO 326
327 STK/AVO 3D VO 6. VO Model Articulations View ScaleRing DoorOpen VO 7. VO 327
328 Satellite Tool Kit STK ,
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