为了寻找能快速准确的完成导弹惯导传递对准的直升机机动方法,文中对直升机的机动特性进行了深入研究,建立六自由度运动动力学模型。通过对比分析几种常见机动方式的特点,结合传递对准要求及直升机实际操纵方法,提出一种新的“S”形变速转弯机动。仿真结果表明,在传递对准中采用此机动方式,对准精度较高,速度较快,满足直升机载导弹传递对准要求,操纵易于实现。

To seek a more rapid and perfect helicopter maneuver for missile inertial navigation transfer alignment, the helicopter maneuver characteristics were deeply studied, and a six-freedom kinetic model was built. By compare and analysis of several common maneuver characteristics, and according to the requirements of transfer alignment and helicopter operation, a new S-shaped maneuver with speed changing swerve was proposed. Simulation results indicate that the maneuver which is rapid and achieves perfect alignment and convenient operation, can well meet the requirements of airborne missile transfer alignment.