Development of an Unmanned Coaxial Rotorcraft for the DARPA UAVForge Challenge

Author:

Lin Feng1,Ang Kevin Z. Y.1,Wang Fei1,Chen Ben M.1,Lee Tong H.1,Yang Beiqing1,Dong Miaobo1,Dong Xiangxu1,Cui Jinqiang1,Phang Swee King1,Wang Biao1,Luo Delin1,Peng Kemao1,Cai Guowei1,Zhao Shiyu1,Yin Mingfeng1,Li Kun1

Affiliation:

1. UAV Research Group, the National University of Singapore, Singapore 117576, Singapore

Abstract

In this paper, we present a comprehensive design for a fully functional unmanned rotorcraft system: GremLion. GremLion is a new small-scale unmanned aerial vehicle (UAV) concept using two contra-rotating rotors and one cyclic swash-plate. It can fit within a rucksack and be easily carried by a single person. GremLion is developed with all necessary avionics and a ground control station. It has been employed to participate in the 2012 UAVForge competition. The proposed design of GremLion consists of hardware construction, software development, dynamics modeling and flight control design, as well as mission algorithm investigation. A novel computer-aided technique is presented to optimize the hardware construction of GremLion to realize robust and efficient flight behavior. Based on the above hardware platform, a real-time flight control software and a ground control station (GCS) software have been developed to achieve the onboard processing capability and the ground monitoring capability respectively. A GremLion mathematical model has been derived for hover and near hover flight conditions and identified from experimental data collected in flight tests. We have combined H technique, a robust and perfect tracking (RPT) approach, and custom-defined flight scheduling to design a comprehensive nonlinear flight control law for GremLion and successfully realized the automatic control which includes take-off, hovering, and a variety of essential flight motions. In addition, advanced mission algorithms have been presented in the paper, including obstacle detection and avoidance, as well as target following. Both ground and flight experiments of the complete system have been conducted including autonomous hovering, waypoint flight, etc. The test results have been presented in this paper to verify the proposed design methodology.

Publisher

World Scientific Pub Co Pte Lt

Subject

Control and Optimization,Aerospace Engineering,Automotive Engineering,Control and Systems Engineering

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2. Modeling and GS-PID Control of the Quad-Rotor UAV;Proceedings of the 2018 10th International Conference on Computer and Automation Engineering;2018-02-24

3. High-Precision Multi-UAV Teaming for the First Outdoor Night Show in Singapore;Unmanned Systems;2018-01

4. Modelling and robust control of an unmanned coaxial rotor helicopter with unstructured uncertainties;Advances in Mechanical Engineering;2017-01

5. A framework of frequency-domain flight dynamics modeling for multi-rotor aerial vehicles;Proceedings of the Institution of Mechanical Engineers, Part G: Journal of Aerospace Engineering;2016-08-06

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