The modelling simulation and control of helicopters operating with external loads

Annual Forum Proceedings - AHS International

Volumn II, Issue , 2006, Pages 1022-1035

  Kendrick, Stephen A ^a   Walker, Daniel J ^a  

^a UNIVERSITY OF LIVERPOOL   (United Kingdom)

Author keywords

[No Author keywords available]

Indexed keywords

AIRCRAFT MODELS; CLOSED LOOP CONTROL SYSTEMS; COMPUTER SIMULATION; COMPUTER SOFTWARE; FLIGHT DYNAMICS;

COMMERCIAL SOFTWARE; EXTERNAL LOADS; FLIGHT ENVELOPE; SLUNG LOAD SYSTEMS;

HELICOPTERS;

EID: 33748467592     PISSN: 15522938     EISSN: None     Source Type: Conference Proceeding    
DOI: None     Document Type: Conference Paper

References (16)

1. Sheridan, P.F., "Feasibility Study for Multiple Helicopter Heavy Lift Systems", Vertol Aircraft Corp., Vertol Report. R-136, Philadelphia, PA, Oct 1957.
2. Curtiss, Jr, H.C., Warburton F.W., "Stability and Control of The Twin Lift Helicopter System", Journal of the American Helicopter Society, Vol. 30, No. 2, 1985, pp. 14-23.
3. Ciolani, L.S., and Kanning, G., "Equations of motion of Slung Load Systems with Results for Dual Lift", NASA TM 102246, Feb 1990.
4. Padfield, G.D., White, M.D., "Flight Simulation in Academia; HELIFLIGHT in its first year of operation", The Aeronautical Journal of the Royal Aeronautical Society, Vol 107, No 1075, Sept 2003, pp 529-538.
5. Cicolani, L.S., McCoy, A.M., Tischler, M.B., Tucker, G.E., Gatenio P., Marmar, D., "Flight-Time Identification of a UH-60A Helicopter and Slung Load", NASA Report, NASA/TM1998-112231.
6. anon., Aeronautical Design Standard-33E-PRF, Performance Specification, "Handling Qualities Requirements for Military Rotorcraft", US Army AMCOM, Redstone, Alabama, March 21, 2000.
7. Cooper, G.E. and Harper, R.P., Jr., "The Use of Pilot Ratings in the Evaluation of Aircraft Handling Qualities", 1969, NASA TM D-5133.
8. Cicolani, L.S., "Linear Analysis of a UH60 with Slung Load Suspended with Multi-Cable Sling", Working Paper, November 1996.
9. Ockier C.J., "Evaluation of the ADS-33D Handling Qualities Criteria Using the BO 105 Helicopter", DLR Report, Institut für Flugmechanik, Braunschweig, 1998.
10. Tyson, P.H., Cicolani, L.S., Tischler, M.B., Rosen, A., Levine, D., Gearing, M., "Simulation Prediction and Flight Validation of UH-60A Black Hawk Slung-Load Characteristics", Proceedings, AHS 55th Forum, May 1999.
11. Franklin G.F, Powell J.D, Emami-Naeini A, Feedback Control of Dynamic Systems, third edition, Addison-Wesley Publishing Company, Inc, 1994.
12. Tischler, M.B., Cauffman, B., "Frequency-Response Method for Rotorcraft Identification: Flight applications to BO-105 Coupled Rotor/Fuselage Dynamics". JAHS, Vol. 37, No. 3, July 1992.
13. Tischler, M.B., "System Identification Methods for Aircraft Flight Control Development and Validation", NASA TM 110369, Oct 1995.
14. Hess R.A., Tran P.M., "Pilot/Vehicle Analysis of a Twin - Lift Helicopter Configuration in Hover", American Institute of Aeronautics and Astronautics, Journal of Guidance, Vol. 11, No. 5, Sept-Oct 1988.
15. Menon P.K.A., Prasad J.V.R., Schrage D.P., "Nonlinear Control of a Twin-Lift Helicopter Configuration", American Institute of Aeronautics and Astronautics, Journal of Guidance, Vol. 14, No. 6, Nov-Dec. 1991.
16. Mittal M., Prasad J.V.R., "Three dimensional Modelling and Control of a Twin-Lift Helicopter System", Journal of Guidance, Control, and Dynamics, Vol. 16, No. 1, Jan-Feb1993.