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基于Stateflow的无人机多模态控制转换逻辑设计

朱飞翔 高永 宋汉强

海军航空工程学院学报2017,Vol.32Issue(5):431-437,456,8.
海军航空工程学院学报2017,Vol.32Issue(5):431-437,456,8.DOI:10.7682/j.issn.1673-1522.2017.05.003

基于Stateflow的无人机多模态控制转换逻辑设计

UAV Mult-Mode Control Logic Switching Design Based on Stateflow

朱飞翔 1高永 1宋汉强2

作者信息

  • 1. 海军航空大学,山东烟台264001
  • 2. 海军装备研究院,上海200436
  • 折叠

摘要

Abstract

Aiming at the UAV flight management system model based on Simulink,with the disadvantages of complicated logic and tedious modeling process to full flight state,in this paper,the finite state machine was used to establish the logic switching process of UAV flight control system and various navigation control modes.Finally,combining the flight manage?ment system, the flight control system and the UAV kinematics model, the UAV full state simulation system was estab?lished.Through the simulation,the switching effect of the flight mode of operation was verified.

关键词

有限状态机/无人机/全飞行状态/控制逻辑切换

Key words

state flow/UAV/full flight state/control logic switching

引用本文复制引用

朱飞翔,高永,宋汉强..基于Stateflow的无人机多模态控制转换逻辑设计[J].海军航空工程学院学报,2017,32(5):431-437,456,8.

基金项目

"泰山学者"建设工程专项基金资助项目 ()

海军航空工程学院学报

OACSTPCD

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