远程战术火箭控制方案研究

Study on the control projects of long range tactical rocket

按照由简到繁的顺序,提出三种控制方案并进行了弹道控制仿真计算,分析了各方案的弹道精度,研究适合远程战术火箭弹的控制方案及设计要求,并考察了固体姿控发动机作为执行机构的可行性,认为其具有不少优点,可以满足远程战术火箭的技术要求,但其质量仅略重于空气舵。

Based on the imitative trajectory caculation, three control projects and their accuracy are investigated to obtain suitable control projects and design requirements for a long range tactical missile. At the same time, the attitude control solid motor as the executive mechanism is studied and the result shows that it has some advantages and can meet the requirements of the long range tactical missile though it may be slightly heavier than the jet vane.