Particle swarm-based micro air launch vehicle trajectory optimization method

• 1. 一种基于粒子群算法的火箭助推段弹道优化方法 [P] . 中国专利： CN114117758A . 2022-03-01
• 2. 一种基于改进量子粒子群算法的微能源网优化调度方法 [P] . 中国专利： CN109523065B . 2021.09.10
• 3. PARTICLE SWARM-BASED MICRO AIR LAUNCH VEHICLE TRAJECTORY OPTIMIZATION METHOD [P] . 美国专利： US2012053764A1 . 2012-03-01

  机译： 基于粒子群的微空发射车轨迹优化方法

• 4. Trajectory optimization method for low flying aircraft, uses reference trajectory and load factor to optimize flight trajectory for prediction horizon [P] . SE522711C2 . 2004-03-02

  机译： 低空飞行器的轨迹优化方法，利用参考轨迹和载荷因子对预测地平线进行优化

• 5. METHOD AND DEVICE FOR THE USE OF EXPLOSIVE HEADS SUBMITTED FROM A LAUNCH VEHICLE TO IDENTIFIED COMBAT OBJECTIVES DURING THE FLIGHT TRAJECTORY OF THE LAUNCHING VEHICLE. [P] . ES2161302T3 . 2001-12-01

  机译： 在发射飞机的飞行轨迹中使用发射头向确定的​​作战目标使用炸弹头的方法和装置。

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• 1. 基于收敛深度控制的运载火箭真空段最优制导方法 [C] . Weifeng Chen ,陈伟锋 ,Zhijiang Shao . 2014中国制导、导航与控制学术会议 . 2014
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