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本文对于用状态方程描述的系统,导出了自适应控制律的可实现的形式。结合飞行器滚动角的自动控制,进行了设计与模拟。结果表明:该系统在各种恶劣条件下,都具有良好的适应性能。
In this paper, the realizable form of adaptive control law is derived for the system described by the state equation. Combined with the automatic control of aircraft rolling angle, the design and simulation are carried out. The results show that the system has good adaptability in all kinds of harsh conditions.