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Study on Precision Improvement of Attitude Control System in Closed Loop Guidance
Author(s): 
Pages: 33-38,45
Year: Issue:  4
Journal: AEROSPACE CONTROL

Keyword:  姿控系统积分控制稳定裕度;
Abstract: 为满足闭路制导对姿态跟踪精度的要求,本报告提出了一种新的控制方案,即具有积分性质的姿态控制方案,对其进行了详细的理论分析,并在此方案基础上完成了某型号稳定性分析,进行了数学仿真试验验证,结果表明,在不损失原方案裕度的基础上,姿态偏差得到了有效控制.
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