Evaluation and optimization of strapdown velocity numerical integration algorithms for SINS in spinning ballistic missiles
Author:
Publisher
Springer Science and Business Media LLC
Subject
Metals and Alloys,General Engineering
Link
http://link.springer.com/content/pdf/10.1007/s11771-013-1569-9.pdf
Reference18 articles.
1. BLADES E L, NEWMAN C J. Aeroelastic effects of spinning missiles [C]// Proceedings of the 48th AIAA/ASME/ASCE/AHS/ASC Structures, Structural Dynamics, and Materials Conference. Honolulu, Hawaii, 2007, AIAA Paper 07-2243.
2. ELIAS R, VEGA-NEVAREZ J. Active nutation & precession control for exoatmospheric spinning ballistic missiles [C]// Proceedings of the AIAA Guidance, Navigation and Control Conference and Exhibit, Honolulu, Hawaii, 2008, AIAA Paper 08-6998.
3. SHENG Chun-hua, WANG Xiao, ZHAO Qiu-ying. Aerodynamic analysis of a spinning missile using a high-order unstructured-grid scheme [J]. Journal of Spacecraft and Rockets, 2010, 47(1): 81–89.
4. YAN Xiao-yong, YANG Shu-xing, ZHANG Cheng. Coning motion of spinning missiles induced by the rate loop [J]. Journal of Guidance, Control, and Dynamics, 2010, 33(5): 1490–1499.
5. YAN Xiao-yong, YANG Shu-xing, XIONG Fen-fen. Stability limits of spinning missiles with attitude autopilot [J]. Journal of Guidance, Control, and Dynamics, 2011, 34(1): 278–283
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