利用固体燃气发生器作为控制力源对导弹进行侧向力控制、导弹的末端控制和垂直发射导弹的转弯具有重要的作用。
As control force source, the solid propellant gas generator was used to exert lateral force for the end control and the turn of vertical launching of missiles.
针对战术导弹垂直发射姿态调转时的快速性要求，研究了垂直发射快速姿态调转的次最小时间控制问题。
This paper deals with the near-minimum-time attitude maneuver control of vertical launching tactical missile, in order to solve fast attitude maneuver of this kind of missile.
目的为解决战术导弹自力垂直发射中的燃气排导、防护及防意外点火等问题，提出了一种自力垂直发射系统的新方案；
Aim A new scheme of vertical launching system was presented to solve the problems of combustion gas exhaust and protection, guarding against unexpected firing and so on.
目的为解决战术导弹自力垂直发射中的燃气排导、防护及防意外点火等问题，提出了一种自力垂直发射系统的新方案；
Aim A new scheme of vertical launching system was presented to solve the problems of combustion gas exhaust and protection, guarding against unexpected firing and so on.
应用推荐