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Selecting the loop gains of the unmanned aerial vehicle pitch attitude control system with allowance for tolerances on the aerodynamic and mass centering characteristics

机译：选择无人驾驶飞行器俯仰姿态控制系统的环路，具有对空气动力学和质量定期特征的公差

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Фам Суан Чыонг;
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1. Roll aerodynamic characteristics study of an unmanned aerial vehicle based on circulation control technology [J] . Chen Kun, Shi Zhiwei, Zhu Jiachen, Proceedings of the Institution of Mechanical Engineers . 2019,第3期

机译：基于循环控制技术的无人机侧翻空气动力学特性研究
2. Fuzzy logic based closed-loop strapdown attitude system for unmanned aerial vehicle (UAV) [J] . Hong SK. Sensors and Actuators, A. Physical . 2003,第2期

机译：基于模糊逻辑的无人机姿态闭环捷联系统
3. Ll neural network adaptive fault-tolerant controller for unmanned aerial vehicle attitude control system [J] . Zhou Yan, Liu Huiying, Guo Huijuan, Proceedings of the Institution of Mechanical Engineers . 2021,第13期

机译：LL神经网络自适应容错控制器，用于无人驾驶飞行器姿态控制系统
4. Pitch Attitude Control Design of Unmanned Aerial Vehicle via Hardware-in-the-Loop Simulation [C] . Yun-Ping Sun, Yen-Chu Liang International Conference on Engineering and Technologynnovation . 2013

机译：通过硬件 - 环路仿真的无人空中车辆的音高姿态控制设计
5. Fault Tolerance Analysis of L1 Adaptive Control System for Unmanned Aerial Vehicles. [D] . Krishnamoorthy, Kiruthika. 2015

机译：L1自适应L1自适应控制系统的容错分析。
6. Measurement of Unmanned Aerial Vehicle Attitude Angles Based on a Single Captured Image [O] . Jin Zhang, Lijun Ren, Huaxia Deng, 2018

机译：基于单个捕获图像的无人机姿态角测量
7. Designing adaptive PID controller non-sensitive to changes in aerodynamic characteristics of an unmanned aerial vehicle [O] . Ouissam Boudiba, Sergei Firsov 2019

机译：设计自适应PID控制器对无人机空中车辆的空气动力学特性变化不敏感
8. Human Factors Issues for Controlling Uninhabited Aerial Vehicles: Preliminary Findings in Support of the Canadian Forces Joint Unmanned Aerial Vehicle Surveillance Target Acquisition System Project (Incidence des Facteurs Humains sur le Pilotage des Vehicules Aeriens Telepilotes: Constatations Preliminaires a L'Appui du Projet de Systeme Interarmees D'Acquisition D'Objectif au Moyen de Vehicules Aeriens Telepilotes de Surveillance des Forces Canadiennes) [R] . Arrabito, G. R., Ho, G., Lambert, A., 2010

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Selecting the loop gains of the unmanned aerial vehicle pitch attitude control system with allowance for tolerances on the aerodynamic and mass centering characteristics

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