[1]杨俊春, 倪茂林.基于Riccati方程解的再入飞行器制导律设计[J].航天控制,2006,24(4):31-34.
YANG J C, NI M L.Design of guidance gaw for reentry vehicles based on the solution of Riccati equation[J].Aerospace Control, 2006, 24(4):31-34.
[2]赵汉元.飞行器再入动力学与制导[M]. 长沙:国防科技大学出版社,1997:386.
[3]WANG Y,YU P L.Design of longitudinal predictive reentry guidance law based on variable universe fuzzy-PI composite control[J]. Journal of Control Theory and Applications,2012,10(2):264-267.
[4]ZHANG Z, HU J. Prediction-based guidance algorithm for highlift reentry vehicles[J]. Science China Information Sciences, 2011, 54(3): 498-510.
[5]汤建国,赵汉元.飞船再入制导最佳反馈系数规律[J].国防科技大学学报, 2000,22(3):53-56.
TANG G J,ZHAO H Y. A Study of the optimal feedback gain coefficients of reentry guidance for spacecraft[J].Journal of National University of Defense Technology, 2000 ,22(3):53-56.
[6]梅生伟,申铁龙,刘康志.现代鲁棒控制与应用[M].北京:清华大学出版社,2003:193-214.
[7]XU M l,LIU L H,TANG G J,CHEN K J.Quasi-equilibrium glide autoadaptive entry guidance based on ideology of predictor-corrector[C]//Proceedings of 5th International Conference on Recent Advances in Space Technologies. Istanbul:IEEE,2011:265-269.
[8]曾春平,胡军,孙承启.反馈线性化方法在再入制导中的应用[C] //全国第十二届空间及运动体控制技术学术会议论文集.桂林:自动化学会,2006:280-287.
ZENG C P,HU J,SUN C Q.The application of feedback linearization in reentry guidance[C]//The 12th Technologies of Space and Control of Movement Conference.Guilin Chinese Association of Automation, 2006: 280-287.
[9]胡军,陈祖贵,刘良栋,等.神舟飞船导航制导与控制分系统研制与飞行结果评价[J].航天器工程, 2004,13(4):24-28.
HU J,CHEN Z G,LIU L D,et al.The flight evaluation of the GNC system of Shenzhou spacecraft[J]. Spacecraft Engineering,2004,13(4):24-28. |