Matlab与STK连接函数库最新整理行业二类

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1、整理者：龚德仁2008年10月7日文书#借鉴目 录一、Matlab/Simulink、STK联合仿真的优势1二、mexConnect函数详细介绍22.1 STK服务器命令（STK Server Commands）22.1.1 stkDefaultConID22.1.2 stkDefaultHost22.1.3 stkSetDefaultHost22.2 应用命令（Application Commands）22.2.1 stkAutoSave22.2.2 stkHomeDir22.2.3 stkCurrentDir22.2.4 stkSetCurrentDir22.2.5 stkObjNames

2、22.2.6 stkTimerStart32.2.7 stkTimer32.3 普通对象命令（Generic Object Commands）32.3.1 stkCentralBody32.3.2 stkLoadObj32.3.3 stkSaveObj32.3.4 stkNewObj32.3.5 stkUnload42.3.6 stkUnloadChildren42.3.7 stkRename42.3.8 stkTimePeriod42.3.9 stkTimePeriodInSec52.3.10 stkValidObj52.3.11 stkDescrip52.3.12 stkSetDescri

3、p52.4 场景命令（Scenario Commands）62.4.1 stkAnimTime62.4.2 stkEpoch62.4.3 stkSetEpoch62.4.4 stkSetEpochInSec62.4.5 stkSyncEpoch62.4.6 stkConvertDate62.4.7 stkSetTimePeriod62.4.8 stkSetTimePeriodInSec72.4.9 stkScenFilePath72.4.10 stkValidScen72.5 基本飞行器数据（Basic Vehicle Data）72.5.1 stkTimePeriod72.5.2 stkTi

4、mePeriodInSec72.5.3 stkSetTimePeriod72.6 卫星运动属性（Satellite Propagators）82.6.1 stkSetPropCart82.6.2 stkSetPropClassical82.6.3 stkSetPropEqui92.6.4 stkSetPropSGP492.6.5 stkPropagate102.7 飞行器位置与速度（Vehicle Position and Velocity）102.7.1 stkPosVelCBF102.7.2 stkPosVelCBI102.7.3 stkEphemerisCBF102.7.4 stkEph

5、emerisCBI112.7.5 stkSetEphemerisCBF112.7.6 stkSetEphemerisCBI112.7.7 stkLoadEphemeris112.7.8 stkSaveEphemerisCBF122.7.9 stkSaveEphemerisCBI122.7.10 stkSaveDynState122.7.11 stkDynState122.8 飞行器姿态（Vehicle Attitude）122.8.1 stkAttitudeCBF122.8.2 stkAttitudeCBI132.8.3 stkSetAttitudeCBF132.8.4 stkSetAttit

6、udeCBI132.8.5 stkLoadAttitude142.8.6 stkSaveAttitudeCBF142.8.7 stkSaveAttitudeCBI142.9 基本飞行器姿态类型（Basic Vehicle Attitude Types）142.9.1 stkSetAttBasic142.9.2 stkSetAttSpinSun152.9.3 stkSetAttSpinNadir152.9.4 stkSetAttYawNadir152.9.5 stkSetAttSpinning162.9.6 stkSetAttFixed162.9.7 stkAttOffset172.10 飞机，

7、车辆与船舰属性（Aircraft, GroundVehicle and Ship Propagators）172.10.1 stkSetWaypoints172.10.2 stkLoadWaypoints182.10.3 stkSetGreatArcStart182.11 导弹运动属性（Missile Propagators）182.11.1 stkSetPropBallistic182.12 设备与目标（Facilities and Targets）182.12.1 stkPosVelCBF182.12.3 stkSetFacPosCBF182.12.3 stkSetFacPosLLA192

8、.13 区域目标（Area Targets）192.13.1 Area Target boundary192.14 STK工具（STK Tools）192.14.1 stkAccess192.14.2 stkReport192.14.3 stkAccReport202.14.4 stkFindData212.15 连接命令（Connect Commands）212.15.1 stkOpen212.15.2 stkClose212.15.3 stkExec212.15.4 stkConnect22三、aeroToolbox函数详细介绍223.1 坐标系中的历元与数据函数Coordinate Sy

9、stem Epoch and Date functions）223.1.1 atbGetEpoch223.1.2 atbSetEpoch223.1.3 atbDateToEpochSec233.1.4 atbEpochSecToDate233.2 坐标系转换（Coordinate Conversions）243.2.1 atbCbfToCbi243.2.2 atbCbfToCbiMtx243.2.3 atbCbfToLhMtx243.2.4 atbCbfToLla243.2.5 atbCbfToLlr253.2.6 atbCbfToVvlhMtx253.2.7 atbCbiToCbf253.2

10、.8 atbCbiToCbi263.2.9 atbCbiToCbiMtx263.2.10 atbLlaToCbf263.2.11 atbLlrToCbf273.2.12 atbCbCoordinates273.2.13 atbCoordXForm273.2.14 atbCoordXFormMtx283.3 转动与四元数（Rotations and Quaternions）283.3.1 atbAlignVecQuat283.3.2 atbEulerToMtx283.3.3 atbEulerToQuat293.3.4 atbMinRotQuat293.3.5 atbMtxToEuler293.3

11、.6 atbMtxToQuat293.3.7 atbMtxToYpr303.3.8 atbQuatToMtx303.3.9 atbQuatXquat303.3.10 atbYprToMtx303.3.11 atbYprToQuat313.3.12 atbInterpQuat313.4 中心对象操作与程序（Central Body Operations and Routines）313.4.1 atbCbEphemeris313.4.2 atbCbGetTangent313.4.3 atbCbGravParam323.4.4 atbCbGrazeAlt323.4.5 atbCbGrazeAngl

12、e323.4.6 atbCbIntersect333.4.7 atbCbLclRadCen333.4.8 atbCbLclRadDet333.4.9 atbCbSurfDistCen343.4.10 atbCbSurfDistDet343.4.11 atbCbSurfNormCen343.4.12 atbCbSurfNormDet343.5 指向，星历与姿态文件（Waypoint, Ephemeris and Attitude Files）353.5.1 atbReadAttitudeCBF353.5.2 atbReadAttitudeCBI353.5.3 atbWriteAttitudeCB

13、F353.5.4 atbWriteAttitudeCBI353.5.5 atbReadEphemerisCBF363.5.6 atbReadEphemerisCBI363.5.7 atbWriteEphemerisCBF363.5.8 atbWriteEphemerisCBI363.5.9 atbWriteWaypointFile363.6 位置与速度函数（Position and Velocity Functions）373.6.1 atbGeometry373.6.2 atbGenGreatArc393.6.3 atbCreateDynStateCBF393.6.4 atbCreateDy

14、nStateCBI393.6.5 atbLhQuatCen403.6.6 atbLhQuatCBFDet403.6.7 atbFlatten413.7 轨道要素转换（Orbit Element Set Conversions）413.7.1 atbOrbCartToDel413.7.2 atbOrbCartToEqui413.7.3 atbOrbCartToMod423.7.4 atbOrbCartToSphere423.7.5 atbOrbCartToMixedSphere433.7.6 atbOrbDelToCart433.7.7 atbOrbEquiToCart433.7.8 atbOr

15、bModToCart433.7.9 atbOrbSphereToCart433.7.10 atbOrbMixedSphereToCart433.8 轨道根数分量的转换（Orbit Element Parameter Conversions）433.8.1 atbOrbEccToTrue433.8.2 atbOrbTrueToEcc443.8.3 atbOrbMeanToTrue443.8.4 atbOrbTrueToMean443.8.5 atbOrbLanToRaan443.8.6 atbOrbRaanToLan443.8.7 atbOrbPeriRadToPeriod443.8.8 atb

16、OrbPeriodToPeriRad453.8.9 atbOrbPeriRadToSMajAxis453.8.10 atbOrbSMajAxisToPeriRad453.8.11 atbOrbTPANToTrue453.8.12 atbOrbTrueToTPAN453.8.13 atbOrbTPPToTrue463.8.14 atbOrbTrueToTPP463.9 DTED操作（DTED operations）463.9.1 atbCbListDtedTypes463.9.2 atbCbListDted463.9.3 atbCbAddDtedSource473.9.4 atbCbDtedSo

17、urceUI473.9.5 atbLoadNimaDted473.9.6 atbCbRemDtedSource473.9.7 atbCbGetDtedSourceForPos473.9.8 atbGetDtedPatch483.9.9 atbClearDtedPatch483.9.10 atbAllDtedPatches483.9.11 atbDtedPatchInfo483.9.12 atbDtedElev483.9.13 atbDtedPatchElev493.9.14 atbAzElMask493.9.15 atbDtedRes493.9.16 atbDtedLOSExist493.10

18、 运动属性（Propagators）503.10.1 atbLambertFixedTime503.10.2 atbLambertMinEnergy503.10.3 atbLambertMinEccen503.10.4 atbKeplerProp503.10.5 atbJ2Prop513.10.6 atbJ4Prop513.10.7 atbLaunchProp523.10.8 atbMissilePropDataFixedTime523.10.9 atbMissilePropDataFixedAlt533.10.10 atbMissilePropDataFixedDelta533.10.11

19、atbMissilePropDataMinEnergy533.10.12 atbTLERead533.10.13 atbTLEGetAll543.10.14 atbTLEDelete543.10.15 atbTLEProp543.10.16 atbTLEEpoch543.10.17 atbTLEInfo543.11 导航精度（Navigation Accuracy）553.11.1 atbComputeDOP553.12 地图数据（Map Data）563.12.1 atbMapDetails563.12.2 atbPlotMapDetails563.13 覆盖网格（Coverage Grid

20、s）563.13.1 atbGetPolyHandle563.13.2 atbInsidePoly563.13.3 atbClearPolyHandle57四、stkExec使用总结574.1 场景动画控制574.1.1 控制按钮57五、示例574.1 卫星编队之构型设计574.2 使用心得58一、Matlab/Simulink、STK联合仿真的优势STK/MATLAB,SIMULINK STK与Matlab联合实现可视化仿真集成，该方案可以适用于航空航天、航海、作战模拟、电子对抗、卫星导航定位、遥感遥测、卫星通信等各个可视化仿真集成案例之中。STK/MATLAB接口为STK和MATLAB提供

21、了双向通讯功能，在MATLAB工作区通过Connect模块以TCP/IP协议打开STK端口。 利用超过150个MATLAB命令增强STK的轨道、弹道、轨迹的分析能力，MexConnect还提供在MATLAB命令行直接使用任意 STK/Connect 命令的功能。MexConnect工具可以建立各种不同级别的STK对象，进行操作并生成报告。所有STK的数据，包括动态位置、速度和姿态数据，可以返 回到MATLAB工作空间，用于数学分析。宇航工具箱让MATLAB用户可以输出多重坐标系，以及符合STK格式的星历和姿态文件用于VO模块的三维可视 化。另外此工具还可以使用STK附加模块的功能如STK/CO

22、MM（通信），STK/Coverage （覆盖）和STK/Radar（雷达）。表1 STK模块基本模块基本版专业版三维显示高级三维显示Satellite Tool Kit(STK)STK/Professioal(STKPRO)STK/Visualization Option(STK/VO)STK/Advanced VO分析模块轨道机动链路分析通信分析接近分析覆盖分析拦截飞行工具导弹飞行工具精确定轨雷达分析空间环境STKAstrogatorSTKChainsSTKCommSTKConjunction Analysis ToolsSTKCoverageSTKInterceptor Flight T

23、ool(IFT)STKMissile Flight Tool(MFT)STKPrecision Orbit DeterminationSystem(PODS)STKRadarSTKSpace Environment综合数据高精度数字地图高分辨率地球影像雷达高级环境全球三维地形STKHigh Resolution MapsSTKVO Earth ImagerySTKRadar Advanced Environment(RAE)STKTerrain扩展与接口连接模块网络实时播放MATlLAB接口分布式仿真地理信息接口程序开发库STKConnect and STKServerSTKWebCastST

24、KMATLAB InterfaceSTKDistributed Interactive Simulation(DIS)STKGeographic InformationSystems(GIS)STKProgrammers Library(PL)二、mexConnect函数详细介绍2.1 STK服务器命令（STK Server Commands）2.1.1 stkDefaultConID 作用：返回STK的默认标识2.1.2 stkDefaultHost作用：返回STK的默认地址2.1.3 stkSetDefaultHost作用：设置STK的新地址用法：stkSetDefaultHost(hos

25、t:port)2.2 应用命令（Application Commands）2.2.1 stkAutoSave作用：自动保存STK用法：stkAutoSave(onOff,directory, period) stkAutoSave(onOff)说明：onOff - on or off directory - string pathname of autosave directory period - seconds between saves2.2.2 stkHomeDir作用：返回STK的安装路径用法：dir = stkHomeDir2.2.3 stkCurrentDir作用：返回STK的当

26、前路径用法：dir = stkHomeDir2.2.4 stkSetCurrentDir作用：设置STK的当前路径用法：stkSetCurrentDir(directory)2.2.5 stkObjNames作用：返回STK中对象的名字用法：objNames = stkObjNames objNames = stkObjNames(classCell)说明：classCell - optional cell array of STK class names. objNames - cell array of STK object names 2.2.4 stkSetCurrentDir 2.2

27、.6 stkTimerStart作用：启动计时器用法：stkTimerStart2.2.7 stkTimer作用：返回计时器时间用法：split, total = stkTimer说明：split - elapsed time since last stkTimer command total - elapsed time since last stkTimerStart command2.3 普通对象命令（Generic Object Commands）2.3.1 stkCentralBody作用：返回坐标系的中心体用法：centBody = stkCentralBody(objPath)说

28、明：objPath - String name of object obtained from stkObjNames. If ommitted, the scenario central body is returned. centBody - String name of object coordinate system central body.备注：更多内容参见stkObjNames、aeroToolbox。2.3.2 stkLoadObj作用：导入对象文件用法：stkLoadObj(parentPath, class, fileName) stkLoadObj(scenarioFil

29、eName)说明：parentPath - Valid path, may be obtained from stkObjNames. class - Valid class name. Consult STK documentation for a list of valid classes. Names are case-sensitive. fileName - File path of object file 2.3.3 stkSaveObj作用：将对象保存用法：stkSaveObj(objPath, dirName) stkSaveObj(objPath)说明：objPath - V

30、alid path, may be obtained from stkObjNames. dirName - Directory path of object file. When omitted, the default directory is used.2.3.4 stkNewObj 作用：创建一个新对象用法：stkNewObj(parentPath, class, name)说明：parentPath- Valid path, may be obtained from stkObjNames. class- Valid class name. Consult STK documenta

31、tion for a list of valid classes. Names are case-sensitive. name - Name of new object备注：创建场景时，语法为stkNewObj(Scenario, ,Scenario1)2.3.5 stkUnload作用：卸载对象用法：stkUnload(objPath)说明：objPath- Valid path, may be obtained from stkObjNames.2.3.6 stkUnloadChildren作用：卸载对象的所有子对象用法：stkUnloadChildren (objPath)说明：obj

32、Path- Valid path, may be obtained from stkObjNames.2.3.7 stkRename作用：将对象重命名用法：stkRename(objPath, newName)说明：objPath- Valid path, may be obtained from stkObjNames. newName - New instance name.2.3.8 stkTimePeriod作用：获取对象起止时间用法：timePeriod = stkTimePeriod(dateFormat) timePeriod = stkTimePeriod(objPath, d

33、ateFormat)说明： objPath - Valid vehicle object path, defaults to scenario path.timePeriod - Structure array with start and stop fields. Each field contains a string date value.dateFormat - Valid date format. Options are: EPOCHSEC EPOCHSECOND EPOCHMIN EPOCHMINUTE EPOCHHR EPOCHHOUR EPOCHDAY GMT ZULU GMT

34、SYSTEM GREGLCL GREGORIANLOCAL GREGORIANLCL GREGUTC GREGORIANUTC GREGTAI GREGORIANTAI GREGTDT GREGORIANTDT GREGGPSTIME GREGGPS GREGORIANGPSTIME GPSTIME GPS JULDATE JULIANDATE JULLCL JULIANLOCAL JULIANLCL JULUTC JULIANUTC JUL4 JULIAN4 JULIAN4UTC JDATEOFF JDATEOFFSET JULDATEOFFSET JULEPHEMDATE JULIANEP

35、HEMERISDATE JULIANEPHEM JULTAI JULIANTAI MISELAP MISSIONELAPSED MODJULDATE MODIFIEDJULIANDATE YYDDD YYDDD.DDD YYYYDDD YYYYDDD.HHMMSS YYYYMMDD YYYYMMDD.DDD YYYY/MM/DDTIME YYYY/MM/DD 备注：更对内容参见stkConvertDate、stkObjNames2.3.9 stkTimePeriodInSec作用：获取对象起止时间，以s为单位用法：start, stop = stkTimePeriodInSec(objPath

36、) start, stop = stkTimePeriodInSec说明：objPath - valid object path, see stkObjNames. When not provided, the scenario time period is returned. start, stop - time in seconds2.3.10 stkValidObj作用：检查对象的有效性用法：result = stkValidObj(path)说明：path- object path name result - 1 if valid, 0 otherwise2.3.11 stkDescr

37、ip作用：获取对象的描述用法：description = stkDescrip(objPath, shortLong)说明：objPath- Valid path, may be obtained from stkObjNames. shortLong - Type of description to get, short or long.2.3.12 stkSetDescrip作用：设置对象的描述用法：stkSetDescrip(objPath, shortLong, description)说明：objPath- Valid path, may be obtained from stkOb

38、jNames. shortLong - Type of description to set, short or long. description - Description text.2.4 场景命令（Scenario Commands）2.4.1 stkAnimTime作用：返回当前动画时间用法：time = stkAnimTime说明：time - current STK animation time (sec)2.4.2 stkEpoch作用：返回当前场景历元用法：epoch = stkEpoch(dateFormat)说明：dateFormat- Valid date format

39、.epoch - string representation of scenario epoch. 2.4.3 stkSetEpoch作用：设置场景历元用法：stkSetEpoch(epoch, dateFormat)说明：dateFormat- Valid date format.epoch - string representation of scenario epoch.2.4.4 stkSetEpochInSec作用：设置场景历元用法：stkSetEpochInSec(newEpoch)说明：newEpoch - number of seconds elapsed between cu

40、rrent epoch and the desired epoch.2.4.5 stkSyncEpoch作用：aeroToolbox与STK场景有同样的历元用法：stkSyncEpoch备注：STK and aeroToolbox maintain separate scenario epochs. This function should be called anytime the STK epoch is changed through mexConnect or via the STK GUI.2.4.6 stkConvertDate作用：转换日期格式用法：newDate = stkCo

41、nvertDate(date, format, newFormat)2.4.7 stkSetTimePeriod作用：设置场景或卫星的时间周期用法：stkSetTimePeriod(start, stop, dateFormat) stkSetTimePeriod(satpath, start, stop, dateFormat)说明：satpath - satellite path name, defaults to scenario start, stop- string dates2.4.8 stkSetTimePeriodInSec作用：设置场景的时间周期用法：stkTimePerio

42、dInSec(start, stop)说明：start, stop - time in seconds2.4.9 stkScenFilePath作用：返回场景文件的路径用法：path = stkScenFilePath说明：path - current STK scenario directory2.4.10 stkValidScen作用：检查可用的场景用法：result = stkValidScen说明：result - 1 if valid, 0 otherwise2.5 基本飞行器数据（Basic Vehicle Data）2.5.1 stkTimePeriod作用：获取对象的时间周期用

43、法：timePeriod = stkTimePeriod(dateFormat) timePeriod = stkTimePeriod(objPath, dateFormat)说明：objPath - Valid vehicle object path, defaults to scenario path. timePeriod - Structure array with start and stop fields. Each field contains a string date value.2.5.2 stkTimePeriodInSec作用：获取对象的时间周期用法：start, st

44、op = stkTimePeriodInSec(objPath) start, stop = stkTimePeriodInSec说明：objPath - valid object path, see stkObjNames. When not provided, the scenario time period is returned. start, stop - time in seconds2.5.3 stkSetTimePeriod作用：设置场景或对象的时间周期用法：stkSetTimePeriod(start, stop, dateFormat) stkSetTimePeriod(s

45、atpath, start, stop, dateFormat)说明：satpath - satellite path name, defaults to scenario start, stop- string dates2.6 卫星运动属性（Satellite Propagators）2.6.1 stkSetPropCart作用：设置笛卡尔坐标系下卫星运动的参数用法：stkSetPropCart(objPath, propagator, coordSystem, . tStart, tStop, dt, orbitEpoch, pos, vel, coordEpoch)说明：objPath

46、 - Valid path, may be obtained from stkObjNames. propagator - TwoBody, J2Perturbation, J4Perturbation, HPOP or PODS This parameter is case sensitive! coordSystem - string name of coordinate system, valid choices are: Fixed, J2000, MeanOfDate, MeanOfEpoch, TrueOfDate, TrueOfEpoch, B1950, TEMEOfDate,

47、TEMEOfEpoch, AlignmentAtEpoch. This parameter is case sensitive! tStart, tStop - times in epoch seconds. dt - time step in seconds. orbitEpoch - reference time of orbit data, in scenario epoch seconds pos - 3x1 vector of positions at reference time, meters vel - 3x1 vector of velocity at reference t

48、ime, meters/sec coordEpoch - coordinate system epoch, required by all .OfEpoch coordinate systems.2.6.2 stkSetPropClassical作用：设置经典轨道根数描述下卫星运动的参数用法：stkSetPropClassical(objPath, propagator, coordSystem, . tStart, tStop, dt, orbitEpoch, semimajorAxis, eccentricity,. inclination, argOfPerigree, RAAN, me

49、anAnomaly, coordEpoch)说明：objPath - Valid path, may be obtained from stkObjNames. propagator - TwoBody, J2Perturbation, J4Perturbation, HPOP or PODS This parameter is case sensitive! coordSystem - string name of coordinate system, valid choices are: Fixed, J2000, MeanOfDate, MeanOfEpoch, TrueOfDate,

50、TrueOfEpoch, B1950, TEMEOfDate, TEMEOfEpoch, AlignmentAtEpoch. This parameter is case sensitive! tStart, tStop - times in epoch seconds. dt - time step in seconds. orbitEpoch - reference time of orbit data, in scenario epoch seconds coordEpoch - coordinate system epoch, required by all .OfEpoch coor

51、dinate systems.semimajorAxis - units in meterseccentricity - unitlessinclination - units in radiansargOfPerigree - units in radiansRAAN - units in radiansmeanAnomaly - units in radians2.6.3 stkSetPropEqui作用：设置春分点坐标下卫星运动的参数用法：stkSetPropEqui(objPath, propagator, coordSystem, . tStart, tStop, dt, orbit

52、Epoch, semimajorAxis, . h, k, p, q, meanLongitude, formulation, coordEpoch)说明：objPath - Valid path, may be obtained from stkObjNames. propagator - TwoBody, J2Perturbation, J4Perturbation, HPOP or PODS This parameter is case sensitive! coordSystem - string name of coordinate system, valid choices are

53、: Fixed, J2000, MeanOfDate, MeanOfEpoch, TrueOfDate, TrueOfEpoch, B1950, TEMEOfDate, TEMEOfEpoch, AlignmentAtEpoch. This parameter is case sensitive!tStart, tStop - times in epoch seconds. dt - time step in seconds. orbitEpoch - reference time of orbit data, in scenario epoch seconds coordEpoch - co

54、ordinate system epoch, required by all .OfEpoch coordinate systems. semimajorAxis - units in meters h, k, p, q - unitless meanLongitude - units in radians formulation - string, Posigrade or Retrograde2.6.4 stkSetPropSGP4作用：设置SGP4描述下卫星运动的参数用法：stkSetPropSGP4(objPath, tStart, tStop, dt, tleInfo) stkSet

55、PropSGP4(objPath, tStart, tStop, dt, . SSC, orbitEpoch, meanMotion, . eccentricity, inclination, argOfPerigree. . RAAN, meanAnomaly, meanMotionDot, meanMotionDotDot, bStar)说明：objPath - Valid path, may be obtained from stkObjNames. tStart, tStop - times in epoch seconds. dt - time step in seconds. tl

56、eInfo - tleInfo from atbTLEInfo SSC - U.S. Space Surveillance Center Catalog Number (as a char string) orbitEpoch - string date, must be in YYDDD.SSSSSSS format meanMotion - rev/day eccentricity - unitless inclination - units in radians argOfPerigree - units in radians RAAN - units in radians meanAnomaly - units in radians meanMotionDot meanMotionDotDot bStar - m2/kg2.6.5 stkPropagate作用：设置卫星运动的参数