Design of a UAV Flight Control System Base on Information Fusion

机译：关于信息融合的UAV飞行控制系统设计

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The function and the design of the hardware and software of UAV fight control system are introduced in this paper base on information fusion; the fusion model and main characteristics of the fight control system are analyzed.

机译：本文基于信息融合，将UAV战斗控制系统的硬件和软件的功能和设计介绍;分析了战斗控制系统的融合模型和主要特征。

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《International symposium on test and measurement》|2007年||共2页
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正文语种
中图分类计量学;
关键词
flight control; UAV; modularized design; Information fusion;

机译：飞行控制;无人机;模块化设计;信息融合;

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3. Multivariable adaptive control based consensus flight control system for UAVs formation [J] . Zhen Ziyang, Tao Gang, Xu Yue, Aerospace science and technology . 2019,第Octa期

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4. Design of a UAV Flight Control System Base on Information Fusion [C] . Lili Meng, rnYao Zhao 7th international symposium on test and measurement (ISTM/2007) . 2007

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5. Real-time non-linear flight control of a fixed-wing UAV =REAL-TIME NON-LINEAR FLIGHT CONTROL OF A FIXED-WING UAV [D] . Landry, Mario. 2012

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6. Modeling and Flight Experiments for Swarms of High Dynamic UAVs: A Stochastic Configuration Control System with Multiplicative Noises [O] . Hongbo Zhao, Sentang Wu, Yongming Wen, 2019

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7. Intelligent Flight Control System Design for the Small UAV Based on the Adaptive Neuro-Fuzzy Inference System [O] . Marta M. Komnatska, Dmytro P. Bondarenko 2017

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Design of a UAV Flight Control System Base on Information Fusion

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