[1] |
Sarah N D,Nesrin S K.Survey of planetary entry guidance algorithms[J].Progress in Aerospace Sciences,2014,68:22-28.
|
[2] |
Zhao J,Zhou R,Jin X L.Progress in reentry trajectory planning for hypersonic vehicle[J].Journal of Systems Engineering and Electronics,2014,25(4):627-639.
|
[3] |
Lu P.Predictor-corrector entry guidance for low-lifting vehicles[J].Journal of Guidance Control and Dynamics,2008,31(4):1067-1075.
|
[4] |
梁子璇,任章.基于在线气动参数修正的预测制导方法[J].北京航空航天大学学报,2013,39(7):853-857. Liang Z X,Ren Z.Predictive reentry guidance with aerodynamic parameter online correction[J].Journal of Beijing University of Aeronautics and Astronautics,2013,39(7):853-857(in Chinese).
|
[5] |
Jorris T R,Cobb R G.Three-dimensional trajectory optimization satisfying waypoint and no fly zone constraints[J].Journal of Guidance Control and Dynamics,2009,32(2):551-572.
|
[6] |
谢愈,刘鲁华,汤国建,等.多约束条件下高超声速滑翔飞行器轨迹优化[J].宇航学报,2011,32(12):2499-2504. Xie Y,Liu L H,Tang G J,et al.Trajectory optimization for hypersonic glide vehicle with multi-constraints[J].Journal of Astronautics,2011,32(12):2499-2504(in Chinese).
|
[7] |
Zhao J,Zhou R.Reentry trajectory optimization for hypersonic vehicle satisfying complex constraints[J].Chinese Journal of Aeronautics,2013,26(6):1544-1553.
|
[8] |
Zhao J,Zhou R,Jin X L.Reentry trajectory optimization based on a multistage pseudospectral method[J].Scientific World Journal,2014,878193:1-13.
|
[9] |
雍恩米,钱炜祺,唐伟,等.考虑禁飞圆的滑翔式机动弹道与气动特性参数耦合设计[J].航空学报,2013,34(1):66-75. Yong E M,Qian W Q,Tang W,et al.Coupled design of maneuver glide reentry trajectory and aerodynamic characteristic parameters considering no-fly zone[J].Acta Aeronautica et Astronautica Sinica,2013,34(1):66-75(in Chinese).
|
[10] |
张科南,周浩,陈万春.高超声速飞行器多约束多种机动突防模式弹道规划[J].弹道学报,2012,24(3):85-90. Zhang K N,Zhou H,Chen W C.Trajectory planning for hypersonic vehicle with multiple constraints and multiple maneuvering penetration strategies[J].Journal of Ballistics,2012,24(3): 85-90(in Chinese).
|
[11] |
Xie Y,Liu L H,Tang G J,et al.Highly constrained entry trajectory generation[J].Acta Astronautica,2013,88(1):44-66.
|
[12] |
Xue S B,Lu P.Constrained predictor-corrector entry guidance[J].Journal of Guidance Control and Dynamics,2010,33(4):1273-1281.
|
[13] |
王青,莫华东,吴振东,等.基于能量的高超声速飞行器再入混合制导方法[J].北京航空航天大学学报,2014,40(5):580-585. Wang Q,Mo H D,Wu Z D,et al.Energy-based hybrid reentry guidance for hypersonic vehicles[J].Journal of Beijing University of Aeronautics and Astronautics,2014,40(5):580-585(in Chinese).
|
[14] |
Zhao J,Zhou R,Jin X L.Gauss pseudospectral method applied to multi-objective spacecraft trajectory optimization[J].Journal of Computational and Theoretical Nanoscience,2014,11(10):2242-2246.
|
[15] |
Lu P,Xue S B.Rapid generation of accurate entry landing footprints[J].Journal of Guidance Control and Dynamics,2010,33(3): 756-767.
|