Research and Design of Four Rotor UAV Based on Cascade PID

Author:

Lv Deshen,Liang Chengquan,Zhang Ying

Publisher

Springer Nature Switzerland

Reference23 articles.

1. Chaoqiong, Y., Faqing, W.: Design of STM32 four axis aircraft. Electronic world 01, 187–188 (2022). (in Chinese)

2. Xuanbing, L., Xuanbing, L., Shaolei, Z., Zhicai, X., et al.: Track tracking wind resistance of fixed wing UAV. Mod. Defense Technol. 50(01), 41–47 (2022). (in Chinese)

3. Zhdanov, S., Kadet, N., Silkov, V., et al.: The mathematical model for research of the UAV longitudinal moving. Int. J. Eng. Manufact. (IJEM), 13(5), 29–39 (2021)

4. Fei, D.: Algorithm and software design and implementation of personal navigation system based on MEMS inertial devices. Dongnan University, Nanjing (2017). (in Chinese)

5. Hou, J.: Research on attitude calculation and control system of four axis aircraft. Taiyuan University of Technology,  Taiyuan  (2018) (in Chinese)

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