带有偏流角修正的激光雷达卫星全零多普勒姿态导引策略OA
Total Zero Doppler Attitude Steering Strategy with Drift Angle Correction for LiDAR Satellite
搭载高光谱相机的激光雷达卫星可进行主动、被动联合探测,但需要解决全零多普勒姿态导引方法及姿态导引与偏流角修正相结合的姿态控制策略问题.文章基于导引坐标系推导以卫星位置、速度矢量为参数的全零多普勒姿态导引方法,可完全消除多普勒中心频率残余;建立以矢量形式表示的偏流角计算模型,提出在全零多普勒导引姿态下修正偏流角的姿态控制策略及姿态计算过程,可满足联合探测时主动、被动载荷各自对姿态控制的要求;进一步推导全零多普勒导引姿态下偏流角的近似解析表达式,并分析全零多普勒导引姿态下偏流角随纬度幅角的变化规律及受偏心率等参数影响的情况.针对具体任务场景进行数值仿真,结果证明带有偏流角修正的全零多普勒姿态导引策略及相关分析正确有效.
A LiDAR satellite equipped with hyperspectral cameras is capable of performing active-passive joint detection.However,it is necessary to address the total zero Doppler attitude steer-ing method and the attitude control strategy that integrates attitude steering with drift angle cor-rection.Based on the steering coordinate system,a total zero Doppler attitude steering method parameterized by the satellite position and velocity vectors is derived,which is capable of com-pletely eliminating the residual Doppler centroid frequency.A vector-based drift angle calculation model expressed in vector form is then established,and an attitude control strategy and corre-sponding attitude computation process are proposed to correct the drift angle during the total zero Doppler steering attitude,thereby satisfying the respective attitude control requirements of active and passive payloads during joint detection.Furthermore,an approximate analytical expression of the drift angle during the total zero Doppler steering attitude is derived,and the variation of the drift angle with latitude argument,as well as its dependence on parameters such as orbital ec-centricity is analyzed.Numerical simulations are conducted for a specific mission scenario,and the results demonstrate that the proposed total zero Doppler attitude steering strategy with drift angle correction,as well as the associated analysis,is correct and effective.
张磊;李明虎;赵鸿志
航天东方红卫星有限公司,北京 100094航天东方红卫星有限公司,北京 100094航天东方红卫星有限公司,北京 100094
航空航天
激光雷达卫星星载激光雷达高光谱相机全零多普勒姿态导引偏流角修正
LiDAR satellitespaceborne LiDARhyperspectral cameratotal zero Doppler attitude steeringdrift angle correction
《航天器工程》 2026 (1)
26-36,11
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