A Switching-Free Control Architecture for Transition Maneuvers of a Quadrotor Biplane Tailsitter-Reference-Cited by-同舟云学术

A Switching-Free Control Architecture for Transition Maneuvers of a Quadrotor Biplane Tailsitter

Published:2022-06-08 Issue: Volume: Page:
ISSN:
Container-title:2022 American Control Conference (ACC)
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Author:

McIntosh Kristoff¹,Reddinger Jean-Paul²,Mishra Sandipan¹

Affiliation:

1. Rensselaer Polytechnic Institute, Rensselaer Polytechnic Institute,Center for Mobility with Vertical Lift (MOVE),Troy,NY,12180

2. DEVCOM Army Research Laboratory,MD,USA,21005

Funder

Army Research Laboratory

Office of Naval Research

Arm

Publisher

IEEE

Link

http://xplorestaging.ieee.org/ielx7/9866948/9867142/09867242.pdf?arnumber=9867242

Reference12 articles.

1. Development of Flight Dynamics Model and Control of Biplane-Quadrotor UAV

2. Modeling and trajectory control of a transitioning quadrotor biplane tailsitter;reddinger;Vertical Flight Society 75th Annual Forum Proceedings,2019

3. Robust trajectory tracking control for unmanned tail‐sitters in aggressive flight mode transitions

4. Optimal trajectory generation of a quadrotor biplane tailsitter;mcintosh;Vertical Flight Society 76th Annual Forum Proceedings,2020

5. Adaptive control of the transition from vertical to horizontal flight regime of a quad tailsitter uav;carter;Ph D Dissertation,2021

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1. Aerodynamics-Aware Design and Analysis of Controllers for Tailsitter Vehicles;IEEE/ASME Transactions on Mechatronics;2024-08

2. Aerodynamic Feedforward-Feedback Architecture for Tailsitter Control in Hybrid Flight Regimes;Journal of Guidance, Control, and Dynamics;2024-06-25

3. A Feedback-Feedforward Controller for Hybrid Flight Regimes in Transitioning Aerial Vehicles;2023 American Control Conference (ACC);2023-05-31