2007, Volume 9, Issue 9
Strategic Study of CAE >> 2007, Volume 9, Issue 9
Synthesis of Bi-planar Vertical Guidance and Control for Cruise Missile
1. Beijing Electromechanical Engineering Research Institute, Beijing 100074, China;
2. Dept of Computer, Shandong Finance Institute, Jinan 250014, China
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Abstract
]To meet the cruise missile's air-to-surface attack requirement, specified impact angle guidance law is presented based on line of sight (LOS) information framework. Theoretical analysis proves its property. Considering the missile autopilot's dynamics, a simple engineering version of integrated guidance and control synthesis is deduced to improve performance. Mid-course trajectory characteristic is utilized to obtain smooth and low-delay vertical velocity to calculate trajectory angle. Finally mathematical simulation demonstrates their effectiveness.
Keywords
cruise missile ; line of sight (LOS) ; constrained guidance ; integrated guidance and control
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References
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