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Variable Structure Control for High Speed Reentry Aerocraft and Its Simulation Studies
Author(s): 
Pages: 39-45
Year: Issue:  4
Journal: AEROSPACE CONTROL

Keyword:  再入飞行器制导变结构控制最优化;
Abstract: 针对高速再入飞行器模型的快时变、强耦合及严重非线性的特点,采用变结构控制方法设计了自动驾驶仪;同时,采用最优化设计理论与理想速度曲线相结合的方法,设计了能同时保证末端制导精度及速度方向、大小的制导律.最后,进行了系统六自由度仿真,结果表明:本文设计的制导律及控制方案合理、有效,易于实现.
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