The optimization design problem of controller parameters of optimal on-off times attitude maneuvers with switch moment is investigated.
研究空间飞行器大角度姿态机动反馈开关控制的消振参数优化设计问题。
This kind of gyro calibration is to calculate the constant drifts of gyros using the telemetry data of the sun sensors and the rate integrating gyros through twice attitude maneuvers.
此种陀螺标定需进行两次姿态机动，利用太阳敏感器和速率积分陀螺遥测数据标定陀螺的常值漂移。
In this paper, attitude control problem of a rigid spacecraft with large Angle maneuvers is investigated.
研究了刚体飞行器大角度机动的姿态控制问题。
This method would be applied for the attitude capture and maneuvers control of the satellite at any time when the optimum maneuver trajectory was unknown.
在毋需获知最优机动轨迹规划的情况下，可用于卫星任意时刻的姿态捕获和机动控制。
The problem of attitude tracking maneuvers of satellite is studied with MRPs.
基于MRP参数研究了卫星姿态跟踪问题。
The problem of attitude tracking maneuvers of satellite is studied with MRPs.
基于MRP参数研究了卫星姿态跟踪问题。
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