火力与指挥控制2026，Vol.51Issue(2)：70-80,11.DOI:10.3969/j.issn.1002-0640.2026.02.010
基于导弹典型机动轨迹的建模优化
Modeling and Optimization Based on Typical Missile Maneuvering Trajectories
摘要
Abstract
The mathematical model of cruise missiles is a critical component in air situation simulation.This study focuses on the maneuver trajectory models of cruise missiles for typical maneuvers,including serpentine maneuvers,spiral maneuvers,and altitude-reduction maneuvers,and constructs them in detail and in stages.The transition factors for pitch and heading angles are introduced to achieve a smooth transition from level flight to maneuvering,while acceleration influence factors enable stable variable acceleration during acceleration and deceleration phases.The spiral maneuver trajectory modeling is improved to allow for flexible adjustments.Simulation is conducted based on the established maneuver models,making cruise missile flight data intuitive and the trajectory visually clear.The results indicate that the model has been successfully established,providing a valuable reference for digital simulation in the field of cruise missile confrontation simulation.关键词
机动轨迹/巡航导弹/航迹仿真/蛇形机动/螺旋机动/滚筒机动/降高机动Key words
maneuver trajectory/cruise missile/trajectory simulation/serpentine maneuvers/spiral maneuvers/barrel roll maneuver/altitude-reduction maneuvers分类
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张轩铭,刘云清,李晓龙..基于导弹典型机动轨迹的建模优化[J].火力与指挥控制,2026,51(2):70-80,11.
