For nonlinear attitude system of flying vehicle with pure time-delay, inertia and bang-bangcontrol a control method using decoupling variable structure is given.
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。
2
Taking the disturbance into consideration, derives a group of equation used to calculate the on-off curves. By means of the on-off curves, steady process may be realized by the bang-bangcontrol.
本文考虑了扰动因素，推导出一组算式，利用计算得出的开关曲线，可实现开关控制法的稳定控制。
3
First, a linear control scheme is discussed and then a bang-bang...