The attitude tracking maneuvers of spaceborne spotlight SAR

Liqiang. Xu, Junli Chen, Guozhong Chen, Xiaowei Shao, D. Duan
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引用次数: 2

Abstract

The spotlight mode of spaceborne SAR platforms often have to point its payload to immobile target on the ground which means the satellite attitude have to follow a specific trajectory in a fixed time span. In this paper, the attitude angle, angular velocities and angular accelerate are derived. A PD control law with feedforward is developed to achieve the purpose. The approach is verified using numerical simulation with external disturbance and uncertain model.
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星载聚光SAR的姿态跟踪机动
星载SAR平台的聚束模式往往需要将其有效载荷指向地面上的固定目标,这意味着卫星姿态必须在固定的时间跨度内遵循特定的轨迹。本文推导了姿态角、角速度和角加速度。为此,提出了一种带前馈的PD控制律。通过具有外部干扰和不确定模型的数值仿真验证了该方法的有效性。
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