|
|
High Dynamic Decoupling Method of Strapdown Photoelectric Seeker |
CHEN Bing,LI Keyong,CHEN Guoliang |
Shanghai ElectroMechanical Engineering Institute, Shanghai 201109, China |
|
|
Abstract In this paper, the implementation method of mini missile proportional guidance guided by combination of the strapdown photoelectric seeker and MEMS inertial measurement unit is studied; and a method of extracting lineofsight angular velocity by using mathematical decouping algorithm and the least square fitting is proposed. Numerical simulations show that the method has good performance in suppressing measurement noise and counter attitude disturbance. Compared with the conventional virtual tracking loop decoupling, the proposed method has higher output accuracy of line-of-sight angular velocity.
|
Received: 21 December 2018
Published: 08 January 2020
|
|
|
|
|
[1] |
ZHAO Bin, HUANG Xiaoyang, ZHOU Jun, GUO Yue. Multi-missile Distributed LOS Cooperative Guidance Law Design Based on Sliding Mode Control[J]. Air & Space Defense, 2020, 3(3): 16-23. |
[2] |
LIU Yue, ZHANG Jialiang, ZHAO Lijuan, ZHEN Ziyang. Research on Multi-missile Cooperative Guidance Law Based on Second-order Sliding Mode Control[J]. Air & Space Defense, 2020, 3(3): 83-88. |
[3] |
FU Lei, ZHANG Long, ZHANG Ding. Research on High-speed Maneuvering Target Motion State Estimation Algorithm Based on IMM-SRCDKF[J]. Air & Space Defense, 2020, 3(1): 50-57. |
[4] |
ZHAO Bin, ZHU Chuanxiang, TONG Yun, HU Yang, JIANG Ruimin. Adaptive Sliding Mode Observer Based Impact Angle Constraint Guidance Law[J]. Air & Space Defense, 2019, 2(4): 19-24. |
[5] |
HUANG Luyu, XU Shengli, ZHANG Minghuan. Canard/Tail Rudder Compound Control Technology Based on Sequential Quadratic Programming [J]. Air & Space Defense, 2019, 2(3): 38-43. |
[6] |
SHU Chuanliang, ZHU Di, ZHONG Yongjian, MENG Wanli, HAO Lianying. Design of Midcourse Guidance Law of Air Defence Missile Intercepting High Speed Maneuvering Target with Big Diving Angle[J]. Air & Space Defense, 2019, 2(1): 29-32. |
|
|
|
|