Analysis of Classical and Alternate Hexacopter Configurations with Single Rotor Failure
Author:
Affiliation:
1. Rensselaer Polytechnic Institute, Troy, New York 12180
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Aerospace Engineering
Link
https://arc.aiaa.org/doi/pdf/10.2514/1.C035005
Reference6 articles.
1. Design of a Multi Rotor MAV with regard to Efficiency, Dynamics and Redundancy
2. Controllability Analysis and Degraded Control for a Class of Hexacopters Subject to Rotor Failures
3. Relaxed hover solutions for multicopters: Application to algorithmic redundancy and novel vehicles
4. Multirotor Controls, Trim, and Autonomous Flight Dynamics of Plus- and Cross-Quadcopters
5. Control and Performance of a Reconfigurable Multicopter
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