At hypersonic speed, strong nonlinear couplings will bring enormous challenges to the
attitude control of a hypersonic flight vehicle. To reduce the negative impacts of the …

A command filtered back-stepping attitude controller is exploited and analyzed to design a
dynamic state-feedback controller for a generic Reentry Vehicle. A novel back-stepping …

针对变构型多操纵面可重复使用飞行器(RLV) 的进场着陆问题, 提出了一种进场着陆轨迹设计
方法. 将进场着陆轨迹分为深下滑着陆轨迹和拉平着陆轨迹; 考虑了气动舵面可操纵偏转限制及 …

Near space vehicle (NSV) is a nonlinear, multivariable and strongly coupled system. During
the arbitrary trajectory tracking of NSV, the employment of conventional sliding mode …

A command filtered back-stepping technology is exploited and analyzed to design a
dynamic statefeedback attitude controller for a generic reentry vehicle in the technical notes …

The paper is devoted to develop launch vehicle (LV) motion control algorithms for solution of
the two special control problems at the initial flight part: controlled engines plumes …

To solve approach and landing problem of variable configuration reusable launch vehicle
(RLV) with multi-control surfaces, a design method of approach and landing trajectory was …

针对再入飞行器, 提出一类新型的简洁的指令滤波反步法, 设计动态的状态反馈姿态控制器.
所设计的指令滤波反步控制器中, 构建积分滑模滤波器逼近虚拟控制输入及其导数 …

In this paper, a state dependent Riccati equation-based second order integral sliding mode
control (SSOISMC) algorithm is proposed for the reentry vehicle with a strong coupling …