固定翼无人机飞行参数评估模型与实验  

Fixed-Wing UAV Flight Parameter Evaluation Model and Experiment

作　　者：李欣平 王立峰[1] 李昊晨 Xinping Li;Lifeng Wang;Haochen Li(School of Electrical and Control Engineering,North China University of Technology,Beijing)

机构地区：[1]北方工业大学电气与控制工程学院,北京

出　　处：《建模与仿真》2024年第3期3627-3634,共8页Modeling and Simulation

摘　　要：固定翼无人机飞行过程中,为减小模型参数的不确定性和外界扰动对控制器的影响,本文提出了一种飞行参数估计模型,在STM32上通过编程实现了该模型,通过飞行试验验证了该飞行参数估计模型的可行性。In order to reduce the uncertainty of model parameters and the influence of external disturbances on the controller during the flight of fixed-wing UAV,a flight parameter estimation model was proposed in this paper.The model was implemented through programming on STM32,and the feasibility of the flight parameter estimation model was verified through flight tests.

关 键 词：STM32 固定翼无人机 飞行参数估计模型 

分 类 号：V27[航空宇航科学与技术—飞行器设计]