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Flight-control system for canard-controlled flight vehicles and methods for adaptively limiting acceleration
Flight-control system for canard-controlled flight vehicles and methods for adaptively limiting acceleration
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机译:用于鸭航控制飞行器的飞行控制系统和自适应限制加速度的方法
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摘要
Embodiments of a flight-control system and methods of reducing the probability of a roll-control reversal in a canard-controlled flight vehicle are generally described herein. In some embodiments, the flight-control system may monitor angular velocities of the flight vehicle to detect the onset of instability and adaptively control an acceleration limit of the flight vehicle based on the detected instability to reduce the probability of a roll-control reversal. The onset of instability may be detected by persistently high angular velocities. The acceleration limit may be further adaptively controlled based on an approach of a vehicle trim limit.
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