内容发布更新时间 : 2025/7/4 10:20:04星期一 下面是文章的全部内容请认真阅读。
create a file in the scenario directory named {objName}.a, where objName is derived from the objPath. 2.8.5 stkLoadAttitude 作用：从文件载入姿态 用法：stkLoadAttitude('objPath', 'fileName') 说明：objPath - Valid path, may be obtained from stkObjNames. fileName - file name. 2.8.6 stkSaveAttitudeCBF 作用：保存姿态到文件 用法：stkSaveAttitudeCBF('objPath', timeStep, 'fileName') stkSaveAttitudeCBF('objPath', timeStep, 'fileName', stopTime) 说明：objPath - Valid path, may be obtained from stkObjNames. timeStep - Granularity of time steps (sec). fileName - file name. startTime - start time (sec). stopTime - stop time (sec). 2.8.7 stkSaveAttitudeCBI 作用：保存姿态到文件 用法：stkSaveAttitudeCBI('objPath', timeStep, 'fileName') stkSaveAttitudeCBI('objPath', timeStep, 'fileName', stopTime) 说明：objPath - Valid path, may be obtained from stkObjNames. timeStep - Granularity of time steps (sec). fileName - file name. startTime - start time (sec). stopTime - stop time (sec). startTime, startTime, 2.9 基本飞行器姿态类型（Basic Vehicle Attitude Types） 2.9.1 stkSetAttBasic 作用：设置基本的姿态类型 用法：stkSetAttBasic('satPath', 'attType', offset) 说明：satPath - string name of satellite offset - either an alignOffset or constraintOffset, depending on type (radians) attType - attitude type string. Valid choices are: NADIRECIVEL NADIRECFVEL NADIRSUN NADIRORBIT ECIVELNADIR ECFVELNADIR SUNNADIR SUNECLIPTIC SUNECIZ SUNOCCULT 2.9.2 stkSetAttSpinSun 作用：旋转轴指向太阳 用法：stkSetAttSpinSun('satPath', rate, offset, epoch) 说明：satPath - string name of satellite rate - angular spin rate (rpm) offset - angular (radians) epoch - contr