燃气直接力控制试验系统设计与运动研究  

Design and Motion Research of Gas Direct Force Control Test System

作　　者：牟蓬涛 宋满存[1] 梁赞[1] 杨绪钊 付春雨[1] Mou Pengtao;Song Mancun;Liang Zan;Yang Xuzhao;Fu Chunyu(Beijing Research Insitute of Precise Mechanical and Electronic Control Equipment, Beijing 100076)

机构地区：[1]北京精密机电控制设备研究所

出　　处：《航天制造技术》2019年第4期31-34,共4页Aerospace Manufacturing Technology

摘　　要：设计了一种侧向小型多燃气喷管直接力控制试验系统。结构上兼顾了喷管的多数量均布性,并具有很强的协调性;同时既可以在系统上直接进行喷管力学特性的测试,又可以开展控制算法验证的运动研究试验,解决了直接力控制系统的设计、测试与验证的关键技术,在直接力控制系统设计方面具有创造性和前沿性。This paper have designed a lateral small multi-gas nozzle direct force control test system. The structure takes into account the multi-quantity uniformity of the nozzle and has strong coordination;at the same time, the mechanical properties of the nozzle can be directly tested on the system;and the motion research test can be carried out by the control algorithm verification.This design solves the key technologies of design, test and verification of direct force control systems, and is creative and cutting-edge in the design of direct force control systems.

关 键 词：侧向小型多燃气喷管 直接力控制试验系统 运动研究 

分 类 号：V249.1[航空宇航科学与技术—飞行器设计] V448