| Citation: | SUN Chun-zhen, HUANG Yi-min, GUO Suo-feng. Reusable launch vehicle pitch attitude control system research by trajectory linearization[J]. Journal of Aerospace Power, 2008, 23(10): 1921-1926. |
| [1] |
Moore T E.Space shuttle entry terminal area energy management[R].NASA-TM-104744,1991.
|
| [2] |
Carman G L.Shuttle TAEM guidance and flight control[R].NASA-TM-81100,1980.
|
| [3] |
孙春贞,黄-敏.重复使用运载器末端能量管理段制导系统仿真[J].系统仿真学报,2007,19(6):1260-1264.SUN Chunzhen.HUANG Yimin.Terminal area energy management guidance scheme simulation for reusable launch vehicle[J].Journal of System Simulation,2007,19(6):1260-1264.(in Chinese)
|
| [4] |
Zhu J J,Banker B D.X-33 ascent flight control design by trajectory linearization-A singular perturbation approach JR].AIAA-2000-4159.
|
| [5] |
WU Xiaofei.A nonlinear flight controller design for a UFO by trajectory linearization method Part I--Modeling[C]//Proceedings of the Thirty-Fourth Southeastern Symposium on System Theory,[S.1.];[s.n.],2002:97-102.
|
| [6] |
WU Xiaofei.A nonlinear flight controller design for a UFO by t raiectory linearization method PartⅡController design[C]//Proceedings of the Thirty-Fourth Southeastern Symposium on System Theory,[s.I.];[s.n.],2002:103-107.
|
| [7] |
Zhu J J.A type two troscetory linearization controller for a reusable launch vehicle-A singular perturbation approach[R].AIAA-2004-5184.
|
| [8] |
Tim B.Improved trajectory linearization flight controller for reusable launch vehicles[R].AIAA-2004-0875.
|
| [9] |
孙春贞,黄-敏,郭锁风.重复使用运载器末端能量管理段轨迹线设计[J],系统工程与电子技术,2007,29(6):909-9 14.SUN Chunzhen,HUANG Yimin,GUO Suofeng.Trajectory design for teminal area energy management of reusable launch vehicle[J].System Engineering and Eelectronics,2007,29(6):909-914.(in Chinese)
|
| [10] |
孙春贞,黄-敏,郭锁凤.无动力自动着陆轨道的鲁棒性分析[J].中国空间科学技术,2006,26(2):24-29.SUN Chunzhen,HUANG Yimin,GUo Suofeng.Robusthess assessing of unpowered autolanding trajectory[J].Chinese Space Science and Technology,2006,26(2):24-29.(in Chinese)
|