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| Research on Big Off-axis Turning Law Under Multiple Constraints for Agile Missile |
| WEI Yali, YIN Wei, LIU Yintian, WANG Xin, HU Chunchao |
| Shanghai Electro-Mechanical Engineering Institute, Shanghai 201109, China |
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Abstract For an agile missile that uses direct lateral force provided by engine plume, under the constraints of turning rapidity, missile speed, expected speed angle and expected attitude angle, this paper designs a turning law employing the optimal axis control principle, the fastest turning rate principle, and the conditions of missile speed limit. Simulation results show that this turning law realizes the turning speed and the turning attitude of the missile, and can guarantee the speed of the missile in flight.
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Received: 30 June 2020
Published: 30 September 2020
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2020, Vol. 3 
