论文信息 - Reusable launch vehicle guidance and control using subspace stabilization control techniques - 字舞流文

Reusable launch vehicle guidance and control using subspace stabilization control techniques

C. Tournes | C. Johnson

[1] Dale F. Enns,et al. Nonlinear control law with application to high angle-of-attack flight , 1992 .

[2] Harvey Gratt,et al. Feedback Linearization Autopilot Design for the Advanced Kinetic Energy Missile Boost Phase , 1995 .

[3] Sahjendra N. Singh,et al. Nonlinear Predictive Control of Feedback Linearizable Systems and Flight Control System Design , 1995 .