Attitude Control of Novel Tail Sitter: Swiveling Biplane–Quadrotor
Author:
Affiliation:
1. Indian Institute of Technology Kanpur, Kanpur, Uttar Pradesh 208 016, India
2. Indian Institute of Technology Bombay, Mumbai, Maharashtra 400 076, India
Funder
Department of Science and Technology, India
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Applied Mathematics,Electrical and Electronic Engineering,Space and Planetary Science,Aerospace Engineering,Control and Systems Engineering
Reference17 articles.
1. Design, Performance and Testing of a Quad Rotor Biplane Micro Air Vehicle for Multi Role Missions
2. Biplane-Quadrotor Tail-Sitter UAV: Flight Dynamics and Control
3. Systematic design methodology for development and flight testing of a variable pitch quadrotor biplane VTOL UAV for payload delivery
4. A Global Strategy for Tailsitter Hover Control
5. Robust control of transition maneuvers for a class of V/STOL aircraft
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