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1
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0029209511
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An investigation of piloting strategies for engine failures during takeoff from offshore platforms
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January
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Thomson, D. G., Talbot, N., Taylor, C., Bradley, R. and Ablett, R. An investigation of piloting strategies for engine failures during takeoff from offshore platforms. Aeronaut. J., 1995, 99(981), January.
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0038535883
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The contribution of inverse simulation to the assessment of helicopter handling qualities
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Proceedings of the 19th ICAS Conference, Anaheim, California, September 1994
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Thomson, D.G.1
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0037859416
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The use of inverse simulation for conceptual design
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16th European Rotorcraft Forum, Glasgow, Scotland, September 1990
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0031701505
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The principles and practical application of helicopter inverse simulation
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0005006733
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Aeronautical Design Standard ADS 33D, United States Army Aviation and Troop Command, July
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Handling Qualities Requirements for Military Rotorcraft. Aeronautical Design Standard ADS 33D, United States Army Aviation and Troop Command, July 1994.
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Handling Qualities Requirements for Military Rotorcraft
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6
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0038197154
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A documentation note on the helicopter inverse simulation package: HELINV
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Internal Report 8814, Department of Aerospace Engineering, University of Glasgow
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Thomson, D. G. A documentation note on the helicopter inverse simulation package: HELINV. Internal Report 8814, Department of Aerospace Engineering, University of Glasgow, 1998.
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Thomson, D.G.1
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7
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Deferred-correction optimal control with applications to inverse problems in flight dynamics
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0033698895
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Modification of a helicopter inverse simulation to include an enhanced rotor model
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Doyle, S. and Thomson, D. G. Modification of a helicopter inverse simulation to include an enhanced rotor model. Am. Inst. Aeronaut. Astronaut. J. Aircr., May-June 2000, 37(3).
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Simulation techniques for the study of the manoeuvering of advanced rotorcraft configurations
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PhD thesis, Department of Aeronautical Engineering, University of Glasgow, March
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Rutherford, S. Simulation techniques for the study of the manoeuvering of advanced rotorcraft configurations. PhD thesis, Department of Aeronautical Engineering, University of Glasgow, March 1997.
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Rutherford, S. and Thomson, D. G. Development of a generic inverse simulation algorithm. Internal Report 9410, Department of Aerospace Engineering, University of Glasgow, July 1994.
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0038197152
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Helicopter inverse simulation incorporating an individual blade rotor model
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Rutherford, S. and Thomson, D. G. Helicopter inverse simulation incorporating an individual blade rotor model. In ICAS Congress, Sorrento, Italy, September 1996, paper 3.6.3.
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ICAS Congress, Sorrento, Italy, September 1996
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The numerical errors in inverse simulation
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Lin, K. C., Lu, P. and Smith, M. The numerical errors in inverse simulation. AIAA-93-3588-CP, 1993.
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Active control of turbulence-induced helicopter vibration
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Anderson, D. Active control of turbulence-induced helicopter vibration. PhD thesis, Department of Aeronautical Engineering, University of Glasgow, March 1999.
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Validation of a non-linear individual blade rotorcraft flight dynamics model using a perturbation method
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0037859420
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Prediction of the dynamic characteristics of helicopters in constrained flight
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Thomson, D. G. and Bradley, R. Prediction of the dynamic characteristics of helicopters in constrained flight. Aeronaut. J., December 1990.
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Modelling and classification of helicopter combat manoeuvres
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