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Flight Control Of A Trirotor Mini-Uav For Enhanced Situational Awareness

Authors: Igor Astrov; Andrus Pedai;

Flight Control Of A Trirotor Mini-Uav For Enhanced Situational Awareness

Abstract

{"references": ["M. R. Endsley, \"Toward a theory of situation awareness in dynamic\nsystems,\" Human Factors, vol. 37, pp. 32-64, March 1995.", "J. Gorman, N. Cooke, and J. Winner, \"Measuring team situation\nawareness in decentralized command and control environments,\"\nErgonomics, vol. 49, pp. 1312-1325, October 2006.", "Interim Brigade Combat Team Newsletter. (Online). Available:\nhttp://www.globalsecurity.org/military/library/ report/call/call_01-18_\ntoc.htm", "S.D. Prior, S.-T. Shen, A.S. White, S. Odedra, M. Karamanoglu, M.A.\nErbil, and T. Foran, \"Development of a novel platform for greater\nsituational awareness in the urban military terrain,\" in Proc. 8th\nInternational Conf. Engineering Psychology and Cognitive Ergonomics,\nSan Diego, USA, 2009, pp. 120-125.", "I. Astrov and A. Pedai, \"Control of hovering manoeuvres in unmanned\nhelicopter for enhanced situational awareness,\" in Proc. International\nConf. Industrial Mechatronics and Automation, Chengdu, China, 2009,\npp. 143-146.", "S. Salazar-Cruz, F.Kendoul, R. Lozano, and I. Fantoni, \"Real-time\ncontrol of a small-scale helicopter having three rotors,\" in Proc. 2006\nIEEE/RSJ International Conf. Intelligent Robots and Systems, Beijing,\nChina, 2006, pp. 2924-2929.", "S. Salazar-Cruz, F.Kendoul, R. Lozano, and I. Fantoni, \"Real-time\nstabilization of a small three-rotor aircraft,\" IEEE Trans. Aerospace and\nElectronic Systems, vol. 44, pp. 783-794, April 2008.", "D. Krutko, Inverse Problems of Control System Dynamics: Nonlinear\nModels. Moscow: Nauka, 1989.", "L.S. Pontryagin, Ordinary Differential Equations. Moscow: Nauka,\n1974."]}

This paper focuses on a critical component of the situational awareness (SA), the control of autonomous vertical flight for an unmanned aerial vehicle (UAV). Autonomous vertical flight is a challenging but important task for tactical UAVs to achieve high level of autonomy under adverse conditions. With the SA strategy, we proposed a two stage flight control procedure using two autonomous control subsystems to address the dynamics variation and performance requirement difference in initial and final stages of flight trajectory for a nontrivial nonlinear trirotor mini-UAV model. This control strategy for chosen mini-UAV model has been verified by simulation of hovering maneuvers using software package Simulink and demonstrated good performance for fast SA in realtime search-and-rescue operations.

Keywords

situational awareness, trirotor aircraft, Flight control, unmanned aerial vehicle.

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This indicator reflects the "current" impact/attention (the "hype") of an article in the research community at large, based on the underlying citation network.
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