Helicopter and tilt-rotor inverse simulation: Methods, features, problems and cures

31st European Rotorcraft Forum

Volumn 2005, Issue , 2005, Pages

  Bradley, R ^a   Thomson, D G ^b  

^a GLASGOW CALEDONIAN UNIVERSITY   (United Kingdom)

^b UNIVERSITY OF GLASGOW   (United Kingdom)

Author keywords

[No Author keywords available]

Indexed keywords

COMPUTER SIMULATION; FLIGHT DYNAMICS; IDENTIFICATION (CONTROL SYSTEMS); RESEARCH;

RESEARCH TOOLS; ROTORCRAFT INVERSE SIMULATION; RUDIMENTARY HELICOPTERS;

HELICOPTER ROTORS;

EID: 33746602724     PISSN: None     EISSN: None     Source Type: Conference Proceeding    
DOI: None     Document Type: Conference Paper

References (15)

1. Anon. Aeronautical Design Standard, Performance Specification Handling Qualities Requirements for Military Rotorcraft, ADS-33E. US Army Aviation and Missile Command, March 2000.
2. Macdonald, C.A. The Development of an Objective Methodology for the Prediction of Helicopter Pilot Workload, PhD Thesis, Department of Mathematics, Glasgow Caledonian University, Scotland, UK, January 2001
3. Thomson, D.G and Bradley, R. The use of inverse simulation for preliminary assessment of helicopter handling qualities, Aeronautical Journal, pp 287-294, August/September 1997
4. Hess, R. A., Gao, C., A Generalized Algorithm for Inverse Simulation Applied to Helicopter Maneuvering Flight, Journal of the American Helicopter Society, Vol. 16, No. 5, October 1993.
5. Avanzini, G., de Matteis, G., Two-Timescale Inverse Simulation of a Helicopter Model. Journal of Guidance, Control and Dynamics 2001; 24 (2): 330-339.
6. Rutherford, S., Thomson, D.G., Helicopter Inverse Simulation Incorporating an Individual Blade Rotor Model, AIAA Journal of Aircraft, Vol. 34, No. 5, Sept/Oct. 1997
7. Thomson, D.G., Bradley, R., Development and Verification of an Algorithm for Helicopter Inverse Simulation, Vertica, Vol. 14, No. 2, May 1990.
8. Smith, P.R., Functional Control law Design using Exact Non-linear Dynamic Inversion, AIAA Atmospheric Flight Mechanics Conference, 1994
9. Bradley, R., The Flying Brick Exposed: Non-Linear Control of a Basic Helicopter Model, Technical Report, TR/MAT/96-51, 1996.
10. Thomson, D.G., Bradley, R., Prediction of the Dynamic Characteristics of Helicopters in Constrained Flight, The Aeronautical Journal, Dec. 1990.
11. Padfield, G.D., Helicopter Flight Dynamics, Blackwell Science, 2000, ISBN 063205607-X
12. Padfield, G.D., Jones, J.P., Charlton, M., HowellL, S.E., Bradley, R., 'Where does the workload go when pilots attack manoeuvres? An analysis of results from flying qualities theory and experiment', Paper 83, Twentieth European Rotorcraft Forum, Amsterdam, October, 1994
13. st American Helicopter Society Forum, Grapevine, Texas, June, 2005
14. th European Rotorcraft Forum, Bristol, Great Britain, paper 46, September 2002.
15. Bradley, R., Thomson, D.G., Handling qualities and performance aspects of the simulation of helicopters flying mission task elements, Paper 139, Eighteenth European Rotorcraft Forum, Avignon, September, 1992