Author:
Sun Yong,Hou MingZhe,Duan GuangRen,Liang XiaoLing
Publisher
Springer Science and Business Media LLC
Reference23 articles.
1. Luo X, Li J. Fuzzy dynamic characteristic model based attitude control of hypersonic vehicle in gliding phase. Sci China Inf Sci, 2011, 54: 448–459
2. Zhang Z, Hu J. Stability analysis of a hypersonic vehicle controlled by the characteristic model based adaptive controller. Sci China Inf Sci, 2012, 55: 2243–2256
3. Youssef H, Chowdhry R, Lee H, et al. Predictor-corrector entry guidance for reusable launch vehicles. In: Proceedings of AIAA Guidance, Navigation, and Control Conference. Reston: AIAA, 2001. AIAA Paper No. 2001-4043
4. Shen Z J, Lu P. On-board generation of three-dimensional constrained entry trajectories. J Guidance Control Dynamics, 2003, 26: 111–131
5. Shen Z J, Lu P. Dynamic lateral entry guidance logic. J Guidance Control Dynamics, 2004, 27: 949–959
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