Flight Evaluation of an Adaptive Velocity Command System for Unmanned Helicopters

Author:

Corban John1,Calise Anthony2,Prasad Jvr2,Heynen Gerhard2,Koenig Benedikt2,Hur Jeong2

Affiliation:

1. Guided Systems Technologies Inc.

2. Georgia Institute of Technology

Publisher

American Institute of Aeronautics and Astronautics

Reference14 articles.

1. 1"Predator Attrition is Continuing", World News

2. Roundup, Aviation Week and Space Technology, p.22, January27,2003.2Calise, A. J. Prasad, J.V.R., and Corban,J. E.,Flight

3. Output Feedback for High-Bandwidth Control of an Unmanned Helicopter," AIAA Guidance, Navigation, and ControlConference, 2001.5Corban, J.E., et.al. "Flight Evaluation of Adaptive

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1. Autonomous Hovering Proportional-Integral Sliding Mode Controller Design and Its Flight Test Validation for a Small-Scaled Unmanned Helicopter;Journal of Aerospace Engineering;2013-10

2. Non-linear Control of Heave for an Unmanned Helicopter Using a Neural Network;Journal of Intelligent & Robotic Systems;2011-09-22

3. Review of Linear and Nonlinear Controller Designs;Intelligent Systems, Control and Automation: Science and Engineering;2011

4. Open-loop reference models for nonlinear control with applications to unmanned helicopter flight;AIAA Guidance, Navigation, and Control Conference;2010-06-26

5. Adaptive Control Augmentation to Existing Autopilots for Fixed-Wing UAVs;AIAA Guidance, Navigation, and Control Conference;2009-06-14

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