Agile Missile Dynamics and Control

作者: Kevin A. Wise , David J. B. roy

DOI: 10.2514/2.4256

关键词:

摘要: IN aircraft close-in-combat scenarios, a large off-boresight angle targeting capability, or the ability to engage targets in the rear hemisphere, is a signifi cant advantage. Superagility in missiles refers to this capability. Following a successful missile launch and separation, dynamic pressures are often too low for aerodynamic controls to make a quick turn. When the propulsion system ignites, vectoring the thrust (or using reaction jets) can provide this capability, and as the velocity increases, the aerodynamic surfaces become more effective …

参考文章(6)
Kevin A. Wise, Comparison of six robustness tests evaluating missile autopilot robustness to uncertain aerodynamics Journal of Guidance Control and Dynamics. ,vol. 15, pp. 861- 870 ,(1992) , 10.2514/3.20918
Steven R. Wassom, Lawrence C. Faupell, Tim Perley, Integrated aerofin/thrust vector control for tactical missiles Journal of Propulsion and Power. ,vol. 7, pp. 374- 381 ,(1991) , 10.2514/3.23337
Kevin A. Wise, Bank-to-turn missile autopilot design using loop transfer recovery Journal of Guidance Control and Dynamics. ,vol. 13, pp. 145- 152 ,(1990) , 10.2514/3.20528
Duane T. McRuer, Dunstan Graham, Irving Ashkenas, Aircraft Dynamics and Automatic Control ,(1973)
RANDAL DOUGLAS, STEVEN MACKLER, JASON SPEYER, Robust hover control for a short takeoff/vertical landing aircraft Guidance, Navigation and Control Conference. ,(1990) , 10.2514/6.1990-3333