搜索资源列表
MissileSim
- 导弹飞行控制 3自由度动力学仿真 质点运动学仿真(Missile flight control)
复合控制模式制导（滑模加直接力）
- 复合控制模式下的导弹拦截仿真，运用滑模控制方法与直接力相结合的方式(The simulation of missile interception in compound control mode is based on the combination of sliding mode control and direct force)
BTT_test
- 实现BTT导弹的6自由度仿真；使用传统比例导引法及PID控制(6 degrees of freedom simulation of BTT missile; traditional proportional navigation and PID control)
Untitled
- 导弹一般采用“自控 + 自导”的制导体制，卫星侦察信息支持下的导弹打击海上移动目作战过程为: 解算卫星侦察信息，获得目标指示信息;将目标指示信息装订到导弹导引部，发射导弹; 导弹按照预先设定的轨道飞行，到达自控终点位置，末制导雷达开机; 末制导雷达覆盖目标，截获目标信号，对目标定位; 导弹对目标进行自动跟踪飞行，直到命中目标(The missile generally uses "self-control + homing" guidance system, and the
SDRE_2D_Navigation
- 在线计算SDRE，实现二维导弹制导控制，主程序利用S-function编写，整个程序运行可靠(SDRE is calculated online, and two dimensional missile guidance and control is realized. The main program is written in S-function, and the whole program is reliable.)
fortran90
- 某导弹飞行控制算法，值得学习的，fortran90(A Missile Flight Control Algorithms)
书籍
- 包含导弹飞行力学书籍及ppt，导弹制导与控制原理书籍，以及有翼导弹飞行动力学(Includes books on missile flight mechanics and ppt, books on missile guidance and control, and flight dynamics of winged missiles)