Wang Jiaxin, Lin Defu, Qi Zaikang, Lv Yingjie. Effect of strapdown seeker disturbance rejection rate on stability of PNG system[J]. Infrared and Laser Engineering, 2013, 42(10): 2608-2613.
| Citation:
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Wang Jiaxin, Lin Defu, Qi Zaikang, Lv Yingjie. Effect of strapdown seeker disturbance rejection rate on stability of PNG system[J]. Infrared and Laser Engineering, 2013, 42(10): 2608-2613.
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Effect of strapdown seeker disturbance rejection rate on stability of PNG system
- 1.
Department of Aerospace Engineering,Beijing Institute of Technology,Beijing 100081,China;
- 2.
The Second Artillery Equipment Academy,Beijing 100085,China
- Received Date: 2013-02-11
- Rev Recd Date:
2013-03-10
- Publish Date:
2013-10-25
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Abstract
According to the problem of the terminal guidance with a strapdown seeker, the main reason of the disturbance rejection rate was analyzed. The proportional navigation guidance system (PNGs) with the disturbance rejection rate parasitical loop(DRRPL) was established, the uniformly asymptotical stability of PNGs was put forward based on Lyapunov stability theory for the time varying system, restrictions of stabilizing PNGs were analyzed with the passivity approach, and the effect of the disturbance rejection rate on the stability of PNGs was studied. The results show that the uniformly asymptotical stability of PNGs is stricter to realize than DRRPL, while the disturbance rejection rate caused by the imperfect decoupling is uncertain, and the positive feedback of DRRPL is more likely to make PNGs unstable in advance and cause a larger miss distance.
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References
|
[1]
|
|
|
[2]
|
Yao Yu, Zhang Guojiang. Discussion on strapdown imaging guidance system [J]. Infrared and Laser Engineering, 2006, 35(1): 1-6, 54. (in Chinese) |
|
[3]
|
Dowan K, Ryoo C K, Yongho K, et al. Guidance and control for missile with a strapdown seeker [C]//ICCAS, 2011: 969-972. |
|
[4]
|
|
|
[5]
|
Janice C R, James H M, Joel P B, et al. The past, present, and future of electronically-steerable phased arrays in defense application[C]//Aerospace Conference, IEEE, 2008: 1-7. |
|
[6]
|
|
|
[7]
|
|
|
[8]
|
Jia Xiaoyuan, Zhao Chao. New stabilization control and guidance information extract approach with a semi-strap-down structure [J]. Infrared and Laser Engineering, 2011, 40(12): 2474-2479. (in Chinese) |
|
[9]
|
Nesline F W, Zarchan P. Radome induced miss distance in aerodynamically controlled homing missiles [J]. AIAA, 84-1845, 1984: 99-115. |
|
[10]
|
|
|
[11]
|
|
|
[12]
|
Zarchan P. Tactical and Strategic Missile Guidance [M]. 5th ed. Virginia: AIAA Inc, 2007: 11-50, 527-540. |
|
[13]
|
|
|
[14]
|
Bhattacharyya Abhijit, Tiwari P K, Vora P, et al. In flight radome error compensation through simulation test data[C]// AIAA Guidance, Navigation and Control Conference, 2005. |
|
[15]
|
Lin Chunliang, Hsiao Yihsing. Adaptive feedforward control for disturbance torque rejection in seeker stabilizing loop [J]. IEEE Transactions on Control Systems Technology, 2001, 9(1): 108-121. |
|
[16]
|
|
|
[17]
|
Du Yunli, Xia Qunli, Qi Zaikang. Research on effect of seeker disturbance rejection rate with phase lag on stability of parasitical loop [J]. Acta Armamentarii, 2011, 32 (1): 28-32. (in Chinese) |
|
[18]
|
|
|
[19]
|
|
|
[20]
|
Xu Ping, Wang wei, Lin Defu. Effect of seeker isolation on guidance and control of terminal guided projectile [J]. Journal of Ballistics, 2012, 24(1): 17-21. (in Chinese) |
|
[21]
|
|
|
[22]
|
Egushi H, Kubo H. Robust stability of guidance and control system for homing missiles[C]//AIAA 29th Aerospace Sciences Meeting Nevada, 1991. |
|
[23]
|
Feng Chunbo. Study on stability of non-linear time varying system with the passivity approach[J]. Acta Automatica Sinica, 1997, 23(6): 776-781. (in Chinese) |
|
[24]
|
|
|
[25]
|
Qi Zaikang, Xia Qunli. Guided Weapon Control Systems[M]. Beijing: Beijing Institute of Technology, 2003. |
|
[26]
|
|
|
[27]
|
Li Dianpu. Non-linear Control System [M]. Xi'an: Press of Northwestern Polytechnical University, 2009. (in Chinese) |
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