王建锋,臧军,姜殿文,蒋毅.基于模型的矢量喷管控制系统设计[J].航空发动机,2017,43(4):23-29
基于模型的矢量喷管控制系统设计
Design for Vector Nozzle Control System Based on Model
  
DOI:
中文关键词:  矢量喷管控制系统;飞行/推进综合控制;基于模型的设计;模型自动测试  自动代码生成;实时仿真
英文关键词:vector nozzle control system  integrated flight propulsion control  model based design  automatic test for model  auto code generation  real-time simulation
基金项目:国家重大基础研究项目资助
作者单位E-mail
王建锋,臧军,姜殿文,蒋毅 中国航发控制系统研究所江苏无锡214063 wjf020410306@aliyun.com 
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中文摘要:
      为实现矢量喷管控制系统正向研发“V ”字模型,使用基于模型的设计方法开展矢量喷管控制系统的设计和验证。建立了 包含矢量喷管液压机械单元、矢量喷管控制器及矢量偏转运动的矢量喷管控制系统模型,与发动机模型、飞机模型集成用于矢量喷 管控制系统的系统综合设计。使用模型自动测试技术开展数字仿真试验,利用自动代码生成技术和实时仿真技术实现控制软件快 速开发和系统半物理试验,试验结果表明了矢量喷管控制系统设计的正确性、高效性。
英文摘要:
      In order to realize the 野V冶model process of forward development for vector nozzle control system, the design and verification of vector nozzle control system based on model-based design was proposed. The model of vector nozzle control system was built, consisted of hydraulic mechanism unit, controller, and vectoring motion model. The synthesis design of the vector nozzle model, the engine model and the aircraft model was used in system level design. The technology of automatic test for model was used in digital simulation, and auto code generation and real-time simulation was used to implement rapid development of software and semi-physical tests for the control system. The test results show the correctness and the efficiency of the design of vector nozzle control system.
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