【摘要】 基于奇异摄动方法，提出了中远程空－空导弹由爬升段控制、巡航段控制和交接段最小能量控制３部分构成的次优中制导律。根据工程实际要求，给出了简单的、易于实现的中制导律执行算法。结果表明，该制导律较好地满足了中制导段的要求。更多还原

【Abstract】 Based on the singular perturbation theory and feedback linearization methodology, a new guidance is obtained by constructing a composite control law from a climbing phase control, cruising phase control and switching phase control. In order to reduce onboard computation, a simple close loop guidance algorithm is given. Finally, the simulation results of a certain kind of air to air missile is presented. It is shown that application of the new guidance law results in smaller heading errors at handover.更多还原