Entry guidance for the X-33 vehicle

被引:67
作者
Lu, P [1 ]
Hanson, JM
机构
[1] Iowa State Univ, Dept Aerosp Engn & Engn Mech, Ames, IA 50011 USA
[2] NASA, George C Marshall Space Flight Ctr, Flight Mech Guidance Navigat & Control Syst Branc, Huntsville, AL 35812 USA
关键词
D O I
10.2514/2.3332
中图分类号
V [航空、航天];
学科分类号
08 ; 0825 ;
摘要
The entry Eight of the X-33 Advanced Technology Demonstrated is first examined by using a trajectory optimization approach. For closed-loop guidance the nominal entry trajectory is defined by a piecewise linear drag vs an energy profile. Under a nonlinear tracking control law and an onboard drag-profile updating scheme, the vehicle reaches the designated target point accurately. To further meet the stringent heading requirement at this point, a ground-track design method and the corresponding trajectory control law, which can be applied at a distance before the vehicle reaches the target point, are developed. Simulations with the X-33 vehicle and trajectory data demonstrate good performance of the guidance algorithms.
引用
收藏
页码:342 / 349
页数:8
相关论文
共 7 条
[1]  
HARPOLD JC, 1979, J ASTRONAUT SCI, V27, P239
[2]   Entry guidance and trajectory control for reusable launch vehicle [J].
Lu, P .
JOURNAL OF GUIDANCE CONTROL AND DYNAMICS, 1997, 20 (01) :143-149
[3]   SHUTTLE ENTRY GUIDANCE REVISITED USING NONLINEAR GEOMETRIC METHODS [J].
MEASE, KD ;
KREMER, JP .
JOURNAL OF GUIDANCE CONTROL AND DYNAMICS, 1994, 17 (06) :1350-1356
[4]  
REGAN FJ, 1993, AIAA ED SERIES, P38
[5]   REENTRY CONTROL TO A DRAG-VS-ENERGY PROFILE [J].
ROENNEKE, AJ ;
MARKL, A .
JOURNAL OF GUIDANCE CONTROL AND DYNAMICS, 1994, 17 (05) :916-920
[6]  
Vinh N. X., 1980, HYPERSONIC PLANETARY, P26
[7]  
ZHOU JL, 1997, TR92107R2 U MAR SYST