测发控系统方舱结构研究

New Type of Measuring Control System Application Structure Research

把航天装备送入空间的快速发射,对测发控系统提出了便捷、移动要求;目前现役运载火箭测发控系统状态是系统复杂、难以移动,已不适应当前航天装备快速送入空间的发展,为此提出一种新型移动式测发控系统方舱结构模式;该模式采取了遵循设备集成原则,通过使用方舱、线缆铺设、人机工程优化等先进设计理念与方法来实现测发控系统快速、可移动的要求,同时解决了该系统原先存在多方面存在的问题;通过长期对系统方舱结构的研究工作,研发出通过采用"设备集成、线缆集中铺设、人机工程优化、方舱结构为平台"等先进技术的新型移动快速测发控系统方舱结构系统,为实现系统快速、可移动要求提供了技术基础;该系统经过工程使用,实现了新一代运载火箭快速简易测发控的目标。

The space and equipment into the rapid launch of the space, the thickness control system proposed is convenient, mobile re quirements. Currently active carrier rocket measuring control system state is complex, difficult to move, has not adapt to the development of the current space equipments quickly into the space. Therefore put forward a new type of portable measuring control system application structure mode. The pattern to follow the principle of equipment integration, by using the square cabinet, cable laying, advanced man-ma- chine engineering optimization design idea and method for measuring the requirement of control system is rapid, portable, and solve the prob- lems existing in the system is original. Through long-term research on the structure of the system application work, developed by adopting ＂ equipment integration, cable laying, man-machine engineering optimization, the square as a platform＂ advanced technology, such as new mo bile rapid measuring control system application structure system, for the realization of the system requirements for rapid, portable provides technical basis. After engineering using the system, which can realize the fast simple new generation carrier rocket test control target.