An Actuator Allocation Method for a Variable-Pitch Propeller System of Quadrotor-based UAVs
This paper presents a control allocation method for enhancing the attitude following performance and the energy efficiency of a variable-pitch propeller (VPP) system on quadrotor-based unmanned aerial vehicles. The VPP system was modeled according to the blade element momentum (BEM) theory, and an a...
Main Authors: | Ching-Wei Chang, Shengyang Chen, Chih-Yung Wen, Boyang Li |
---|---|
Format: | Article |
Language: | English |
Published: |
MDPI AG
2020-10-01
|
Series: | Sensors |
Subjects: | |
Online Access: | https://www.mdpi.com/1424-8220/20/19/5651 |
Similar Items
-
A Novel Experimental Model and a Drag-Optimal Allocation Method for Variable-Pitch Propellers in Multirotors
by: Victor Manuel Arellano-Quintana, et al.
Published: (2018-01-01) -
Variable Pitch Propeller for UAV-Experimental Tests
by: Maciej Podsędkowski, et al.
Published: (2020-10-01) -
Robust Actuator Fault Detection and Diagnosis for a Quadrotor UAV With External Disturbances
by: Yujiang Zhong, et al.
Published: (2018-01-01) -
Study on Active Fault Tolerant Flight Control Systems for Quadrotor UAV with Actuator Failures
Published: (2018-08-01) -
MODEL OF STABILITY STUDY OF RUDDER ACTUATOR SYSTEM OF MANEUVERABLE UNMANNED AERIAL VEHICLE
by: S. G. Parafes’, et al.
Published: (2016-12-01)