Flight Dynamics Modeling for a Small-Scale Flybarless Helicopter UAV

Author:

Taamallah Skander1

Affiliation:

1. National Aerospace Laboratory (NLR)

Publisher

American Institute of Aeronautics and Astronautics

Reference231 articles.

1. 2DoD, "Flying Qualities of Piloted V/STOL Aircraft," Tech. Rep. Specification MIL-F-83300, 1970.

2. 3Howlett, J. J. "RSRA Simulation Model-Vol. I. Mathematical Model Equations," Tech. Rep. SER-72009, Sikorsky Aircraft, 1974.

3. 4Houck, J. A., Moore, F. L., Howlett, J. J., Pollock, K. S., and Browne, M. M. "Rotor Systems research Aircraft Simulation Mathematical Model," Tech. Rep. NTM 78629, NASA Langley Research Center, 1977.

4. 5Chen, R. T. N. "A Simplified Rotor System Mathematical Model for Piloted Flight Dynamics Simulation," Tech. Rep. NTM 78575, NASA Ames Research Center, 1979.

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1. Development of Unified High-Fidelity Flight Dynamic Modeling Technique for Unmanned Compound Aircraft;International Journal of Aerospace Engineering;2021-05-04

2. A Flight Dynamics Model for a Small-Scale Flybarless Helicopter;Journal of Dynamic Systems, Measurement, and Control;2015-11-18

3. Analytical modeling and verification experiments of small electric helicopters with stabilizers based on the blade-element approach;Transactions of the JSME (in Japanese);2014

4. Flatness Based Trajectory Generation For A Helicopter UAV;AIAA Guidance, Navigation, and Control (GNC) Conference;2013-08-15

5. Low-Order Modeling For A Small-Scale Flybarless Helicopter UAV A Grey-Box Time-Domain Approach;AIAA Atmospheric Flight Mechanics Conference;2012-08-13

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