论文部分内容阅读
对于具有纯延迟、惯性和由开关控制的非线性飞行器姿态系统，本文提出了采用解耦变结构控制的方法。计算机仿真结果表明，本方法行之有效，具有优良的鲁棒性，设计方法简单和易于实现数字控制等优点
For a non-linear aircraft attitude system with pure delay, inertia and switch control, this paper presents a method of using decoupled variable structure control. Computer simulation results show that the method is effective, has excellent robustness, simple design method and easy to realize the advantages of digital control