论文信息 - Theta-D Control Technique for Ascent Phase of Reusable Launch Vehicles - 字舞流文

Theta-D Control Technique for Ascent Phase of Reusable Launch Vehicles

Ming Xin | David Drake | S. N. Balakrishnan

[1] Yuri B. Shtessel,et al. Reusable Launch Vehicle Control in Multiple Time Scale Sliding Modes , 2000 .

[2] Michael Athans,et al. Gain and phase margin for multiloop LQG regulators , 1976, 1976 IEEE Conference on Decision and Control including the 15th Symposium on Adaptive Processes.

[3] Ming Xin,et al. A new method for suboptimal control of a class of nonlinear systems , 2002, Proceedings of the 41st IEEE Conference on Decision and Control, 2002..

[4] David B. Doman,et al. Dynamic Inversion-Based Adaptive/Reconfigurable Control of the X-33 on Ascent , 2002 .

[5] Eric N. Johnson,et al. Limited authority adaptive flight control for reusable launch vehicles , 2003 .

[6] Ming Xin,et al. Nonlinear Missile Autopilot Design with theta - D Technique , 2004 .