Citation: | WANG Jiang, LIN De-fu, Li Quan-yun. Stability analysis of tactical missile autopilots based on vector margin[J].JOURNAL OF BEIJING INSTITUTE OF TECHNOLOGY, 2014, 23(3): 292-298. |
[1] |
Mracek C P, Ridgely D B. Missile longitudinal autopilots: connections between optimal control and classical topologies [C]//AIAA Guidance, Navigation and Control Conference and Exhibit, AIAA 2005-6381,2005: 1-29.
|
[2] |
Fleeman E L. Technologies for future precision strike missile systems,RTO-EN-018. France: NATO, 2001: 1-15.
|
[3] |
Manu Sharma, Eugene Lavretsky. Application and flight testing of an adaptive autopilot on precision guided munitions [C]//AIAA Guidance, Navigation, and Control Conference and Exhibit, AIAA 2006-6568,2006: 1-12.
|
[4] |
Zarchan P. Tactical and strategic missile guidance[M]. 5th ed. Reston, VA: AIAA, 2007.
|
[5] |
Kevin A Wise. Robust stability analysis of adaptive missile autopilots [C]//AIAA Guidance, Navigation, and Control Conference and Exhibit, AIAA 2008-6999,2008: 1-18.
|
[6] |
Raziye Tekin, Özgür Atesoğlu, Kemal Leblebicioğlu. Modeling and vertical launch analysis of an aero and thrust vector controlled surface to air missile [C]//AIAA Atmospheric Flight Mechanics Conference, AIAA 2010-7639,2010: 1-17.
|
[7] |
Florian Holzapfel, Stephan Theil. Advances in aerospace guidance, navigation and control[M]. Berlin: Springer-Verlag, 2011.
|
[8] |
Shaul Gutman, Orly Goldan, Sergey Rubinsky. Guaranteed miss distance in guidance systems with bounded controls and bounded noise[J]. Journal of Guidance, Control, and Dynamics, 2012,35(3): 816-823.
|
[9] |
Yan J J, Li S H, Lou S, et al. A guidance law design based on disturbance observer and backstepping method[J]. Acta Aeronautica et Astronautica Sinica, 2012,33(12):2291-2300.
|
[10] |
Wang Hui, Lin Defu, Qi Zaikang. Design and analysis of missile three-loop autopilot with pseudo-angle of attack feedback[J]. Systems Engineering and Electronics, 2012,34(1): 129-135. (in Chinese)
|
[11] |
Fan Junfang, Lin Defu, Su Zhong, et al. Control of static unstable airframes[J]. Journal of Systems Engineering and Electronics, 2010, 21(6): 1063-1071.
|
[12] |
Qi Zaikang. Guided weapon control systems[M]. Beijing: Beijing Institute of Technology Press, 2003.
|
[13] |
Lin Defu, Wang Hui, Wang Jiang, et al. Autopilot design and guidance law analysis for tactical missile[M].Beijing: Beijing Institute of Technology, 2012. (in Chinese)
|