|
|
|
| Design of Reentry Guidance Law of Hypersonic Vehicle Based on No-Fly Zone Avoidance |
| TIAN Ruocen，ZHANG Qingzhen，GUO Yunhe，CHENG Lin |
| 1. School of Automation Science and Electrical Engineering， Beihang University， Beijing 100191， China；
2. Shanghai Electro-Mechanical Engineering Institute， Shanghai 201109， China；
3. School of Astronautics， Beihang University， Beijing 100191， China
|
|
|
|
|
Abstract 3. School of Astronautics， Beihang University， Beijing 100191， China）
Abstract: In order to solve the reentry guidance law design problem of hypersonic vehicle in complex environment, a design method of no-fly zone avoidance reentry guidance law is proposed aiming at the avoidance requirements of no-fly zone such as terrain, geopolitics and air defense interception in reentry process. The longitudinal guidance law realizes fast trajectory planning based on reentry flight corridor method. The lateral guidance law adopts the line-of-sight angle deviation corridor to realize the no-fly zone avoidance and target tracking, and the online prediction correction guidance module is designed according to the range error. The effectiveness of the longitudinal and lateral guidance laws is verified by numerical simulation. The simulation results show that the process constraint and the no-fly zone constraint can be satisfied.
|
|
Received: 12 May 2021
Published: 12 July 2022
|
|
|
|
|
|
| [1] |
LIN Zhaochen, ZHANG Xinran, LIU Ziyang, HE Fenghua, OUYANG Lei. Deep Learning-Based Hypersonic Vehicle Motion Behavior Recognition[J]. Air & Space Defense, 2024, 7(1): 48-55. |
| [2] |
YAN Honglei, LU Yuan, GUO Jie, TANG Shengjing, LI Xiang. Cluster Cooperative Formation Control Method for Underactuated Hypersonic Vehicle[J]. Air & Space Defense, 2024, 7(1): 56-62. |
| [3] |
DI Ziqi, WANG Xiangyu, WU Shuang, ZHOU Yu. An Algorithm for Trajectory Generation and Prediction of Hypersonic Vehicle Based on Transformer Architecture[J]. Air & Space Defense, 2023, 6(4): 35-41. |
| [4] |
. Current Developments in Foreign Hypersonic Vehicles and Defense Systems[J]. Air & Space Defense, 2023, 6(3): 39-51. |
| [5] |
LIU Shuangxi, WANG Yichong, ZHU Mengjie, LI Yong, YAN Binbin. Research on Differential Game Guidance Law for Intercepting Hypersonic Vehicles with Small Missile-to-Target Speed Ratio[J]. Air & Space Defense, 2022, 5(2): 49-57. |
| [6] |
YANG Shu, QIAN Yunxiao, YANG Ting. Linear Parameter-Varying Integrated Control Law Design for a Hypersonic Vehicle[J]. Journal of Shanghai Jiao Tong University, 2022, 56(11): 1427-1437. |
| [7] |
XIONG Junhui, LI Keyong, LIU Yi, JI Yu. Study on Near Space Defense Technology Development and Penetration Strategy[J]. Air & Space Defense, 2021, 4(2): 82-. |
| [8] |
WANG Haoning, TANG Shengjing, GUO Jie, HUANG Fan. Time-Constrained Reentry Guidance with Dynamic Angle of Attack Profile[J]. Air & Space Defense, 2021, 4(1): 71-76. |
| [9] |
LIU Haodong, ZHANG Qingzhen, GUO Yunhe, MAO Jiawen. Online Identification of Morphing Aircraft Model Parameters Based on Recursive Least Square Method[J]. Air & Space Defense, 2020, 3(3): 103-110. |
| [10] |
HUANG Yi-Qing, WANG Li, SUN Chang-Yin. Non-fragile Optimal H2/LQR Control with Regional Pole Placement for Hypersonic Vehicle[J]. Journal of Shanghai Jiaotong University, 2011, 45(03): 423-428. |
| [11] |
QU Xin,REN Zhang,SONG Jianshuang,WANG Junbo
. Modeling and Disturbance Observer Based Control for a Hypersonic Vehicle
[J]. Journal of Shanghai Jiaotong University, 2011, 45(02): 272-0276. |
| [12] |
SUN Yong，DUAN Guangren，ZHANG Maorui，ZHANG Ze
. Reentry Trajectory Optimization of Hypersonic Vehicle Based on Pseudo Energy
[J]. Journal of Shanghai Jiaotong University, 2011, 45(02): 262-0266. |
|
|
|
|
2022, Vol. 5 
