Achievable Thrust Expansion Control at Current Saturation of Variable-Pitch Propeller for Drones-Reference-Cited by-同舟云学术

Achievable Thrust Expansion Control at Current Saturation of Variable-Pitch Propeller for Drones

Published:2022 Issue:27 Volume:55 Page:247-252
ISSN:2405-8963
Container-title:IFAC-PapersOnLine
language:en
Short-container-title:IFAC-PapersOnLine

Author:

Naoki Yuto,Yokota Kentaro,Nagai Sakahisa,Fujimoto Hiroshi

Publisher

Elsevier BV

Subject

General Medicine

Reference12 articles.

1. A novel experimental model and a drag-optimal allocation method for variable-pitch propellers in multirotors;Arellano-Quintana;IEEE Access,2018

2. Analysis and control of a variable-pitch quadrotor for agile flight. Journal of Dynamic Systems, Measurement and Control;Cutler;Transactions of the ASME,2015

3. MUWA: Multi-field universal wheel for air-land vehicle with quad variable-pitch propellers;Kawasaki,2013

4. A study of Range Extension Control System by Optimization of Motor Torque and Propeller Pitch Angle for Electric Airplane;Kobayashi;Technical Meeting on Industrial Instrumentation and Control,2013

5. Development and Thrust Response Evaluation of a Variable Pitch Propeller Quad Tilt-rotor Drone;Komizunai;Transactions of the Society of Instrument and Control Engineers,2020

Cited by 2 articles. 订阅此论文施引文献订阅此论文施引文献，注册后可以免费订阅5篇论文的施引文献，订阅后可以查看论文全部施引文献

1. Tuning PID Control Parameters: A Combined Experimental and Simulation Study;2024 International Conference on Control, Automation and Diagnosis (ICCAD);2024-05-15

2. Mode-Switching Algorithm to Improve Variable-Pitch-Propeller Thrust Generation for Drones Under Motor Current Limitation;IEEE/ASME Transactions on Mechatronics;2023-08