Progress and Prospect of Research on Guidance and Control Technology of Aerospace Vehicle

被引：0
作者：
Yao D.-Q. [1 ,2 ]
Wei Y.-Y. [3 ]
Yang Z.-H. [4 ]
Cui N.-G. [1 ]
机构：
[1] School of Astronautics, Harbin Institute of Technology, Harbin
[2] Beijing Aerospace Technology Institute, Beijing
[3] China Aerospace Science and Industry Corporation, Beijing
[4] HIWING Technology Academy of CASIC, Beijing
来源：
| 1600年 / China Spaceflight Society卷 / 41期
关键词：
Aerospace vehicle; Dynamics modeling; Navigation and Control; Trajectory optimization and guidance;
D O I：
10.3873/j.issn.1000-1328.2020.07.003
中图分类号：
V211 [空气动力学]; V411 [空气动力学];
学科分类号：
0801 ; 080103 ; 080104 ;
摘要：
Based on the brief introduction to the development of the guidance and control technology of aerospace vehicle, aiming at the challenges brought by its typical mission, this paper expounds the key technologies from four aspects, i.e. dynamics modeling, trajectory optimization and guidance, flight control and navigation, and discusses the development of the guidance and control technology of aerospace vehicle. © 2020, Editorial Dept. of JA. All right reserved.
引用
收藏
页码：850 / 859
页数：9
相关论文
共 52 条
  • [1] Baris F, Maj M, Petros A I., Flight dynamics and control of air-breathing hypersonic vehicle: review and new directions, The 12th AIAA International Space Planes and Hypersonic Systems and Technologies, (2003)
  • [2] Han Peng-xin, Research on the navigation guidance and control of reusable boost vehicle, (2011)
  • [3] Chavez F R, Schmidt D K., Analytical aeropropulsive/aeroelastic hypersonic vehicle model with dynamic analysis, Journal of Guidance,Control,and Dynamics, 17, 6, pp. 1308-1319, (1994)
  • [4] Shaughnessy J D, Pinckney S Z, McMinn J D, Et al., Hypersonic vehicle simulation model: winged-cone configuration, (1944)
  • [5] Andrea S, Doman B., Control-oriented modeling of an air-breathing hypersonic vehicle, Journal of Guidance, Control, and Dynamics, 30, 3, pp. 856-869, (2007)
  • [6] Karlgaard C D, Tartabini P V, Blanchard R C, Et al., Hyper-X post-flight trajectory reconstruction, Journal of Spacecraft and Rockets, 43, 1, pp. 105-115, (2006)
  • [7] Prasanna H, Ghose D, Bhat M, Et al., Interpolation-aware trajectory optimization for a hypersonic vehicle using nonlinear programming, AIAA Guidance, Navigation, and Control Conference and Exhibit, (2005)
  • [8] Ryan G W, David R D., Evaluation of several agility metrics for fighter aircraft using optimal trajectory analysis, Journal of Aircraft, 32, 4, pp. 732-738, (1995)
  • [9] Fu Yu, Ma Yong-qing, Cui Nai-gang, Reserch on optimal trajectory of reusable boost vehicle, Journal of Ballistic, 23, 4, pp. 5-9, (2001)
  • [10] Fu Yu, Wang Peng, Cui Nai-gang, Trajectory optimization for reentry vehicle based on sequential gradient-restoration algorithm, Journal of Ballistic, 24, 3, pp. 36-42, (2012)
123456