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.
韦亚利, 殷玮, 刘印田, 王鑫, 胡春朝. 多约束下的敏捷导弹大离轴转弯规律研究[J]. 空天防御, 2020, 3(3): 96-102.
WEI Yali, YIN Wei, LIU Yintian, WANG Xin, HU Chunchao. Research on Big Off-axis Turning Law Under Multiple Constraints for Agile Missile. Air & Space Defense, 2020, 3(3): 96-102.
