A Method for Design of Feedback Control To Limit Missile Dispersion
Author:
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
General Engineering
Link
http://arc.aiaa.org/doi/pdf/10.2514/3.55807
Reference11 articles.
1. Angle-of-Attack Control of Spinning Missiles
2. Angle-of-Attack Control of Drag for Slender Re-entry Vehicle Recovery
3. Impact dispersion due to mass and aerodynamic asymmetries.
Cited by 4 articles. 订阅此论文施引文献 订阅此论文施引文献，注册后可以免费订阅5篇论文的施引文献，订阅后可以查看论文全部施引文献
1. Multiple-input describing function technique applied to design a single channel ON-OFF controller for a spinning flight vehicle;Proceedings of the Institution of Mechanical Engineers, Part G: Journal of Aerospace Engineering;2012-06
2. Control of missile dispersion via roll rate modulation;Journal of Guidance, Control, and Dynamics;1986-11
3. Control of missile dispersion via roll rate modulation;12th Atmospheric Flight Mechanics Conference;1985-08-17
4. Lift-Dispersion Control of Spinning Re-entry Vehicles;Journal of Guidance and Control;1980-11
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