Hostname: page-component-cb9f654ff-kl2l2 Total loading time: 0 Render date: 2025-08-23T11:42:55.214Z Has data issue: false hasContentIssue false
  • English
  • Français

An investigation of piloting strategies forengine failures during takeoff from offshoreplatforms

Part of: 75 year anniversary of Aeronautical Engineering at Glasgow University

Published online by Cambridge University Press:  04 July 2016

D. G. Thomson ,
C. D. Taylor ,
N. Talbot ,
R. Ablett  and
R. Bradley
D. G. Thomson
Affiliation:
Department of Aerospace Engineering , University of Glasgow
C. D. Taylor
Affiliation:
Department of Aerospace Engineering , University of Glasgow
N. Talbot
Affiliation:
Civil Aviation Authority, Gatwick
R. Ablett
Affiliation:
Civil Aviation Authority, Gatwick
R. Bradley
Affiliation:
Glasgow Caledonian University
Get access Rights & Permissions [Opens in a new window]

Summary

An analysis technique capable of simulating the effectof engine failure during takeoff from offshoreplatforms is presented. Use is made of inversesimulation whereby the control actions required fora subject helicopter to follow a particulartrajectory can be established. A mathematicalrepresentation of the towering takeoff procedure,and details of the modified inverse simulationtechnique needed to cope with the modelling of anengine failure are described. Detailed pilotingaccounts of the strategy used to fly the toweringtakeoff (with and without engine failures) are alsogiven and are used to give qualitative validation ofthe analytical approach. Simulation results for asingle engine failure of a transport helicopterduring critical phases of a towering takeoff arepresented. Finally, some directions for future workand potential applications of the technique arediscussed.

Information

Type
Research Article
Information
The Aeronautical Journal , Volume 99 , Issue 981 , January 1995 , pp. 15 - 25
Copyright
Copyright © Royal Aeronautical Society 1995 

Access options

Get access to the full version of this content by using one of the access options below. (Log in options will check for institutional or personal access. Content may require purchase if you do not have access.)

Article purchase

Temporarily unavailable

References

1. Thomson, D.G., and Bradley, R. Development and verification of an algorithm for helicopter inverse simulation, Vertica, May 1990, 14, (2), pp 185-200.Google Scholar
2. Bradley, R., Padfield, G.D., Murray-Smith, D.J., and Thomson, D.G. Validation of helicopter mathematical models, Trans Inst Measurement Control, 1990,12, (4), ppl 86-196.Google Scholar
3. Thomson, D.G. An analytical method of quantifying helicopter agility. Paper 45, Proceedings of the 12th European Rotorcraft Forum, Garmisch-Partenkirchen, Federal Republic of Germany, September 1986.Google Scholar
4. Thomson, D.G. and Bradley, R. The development and potential of inverse simulation for the quantitative assessment of helicopter handling quantities. In: Proceedings of the AHS/NASA Conference Piloting Vertical Flight Aircraft: Flying Qualities and Human Factors, San Francisco, January 1993.Google Scholar
5. British Civil Airworthiness Requirements Part 29, Civil Aviation Authority.Google Scholar
6. Anon, Aeronautical Design Standard, Handling Qualities Requirements for Military Rotorcraft, ADS-33C, August 1989.Google Scholar
7. Thomson, D.G. and Bradley, R. Modelling and classification of helicopter combat manoeuvres. Paper 5.9.1, Proceedings of the 17th ICAS Conference, September 1990.Google Scholar
8. Thomson, D.G. Development of a Generic Helicopter Mathematical Model for Application to Inverse Simulation, University of Glasgow, Department of Aerospace Engineering, Internal Report 9216, June 1992.Google Scholar
9. Taylor, C, Thomson, D.G. and Bradley, R. Rotor inflow modelling enhancements to helicopter generic simulation mathematical model, University of Glasgow, Department of Aerospace Engineering, Internal Report 9215, September 1992.Google Scholar
10. Taylor, C, Thomson, D.G. and Bradley, R. The simulation of recovery procedures from engine failures during helicopter offshore operations, University of Glasgow, Department of Aerospace Engineering, Internal Report 9310, July 1993.Google Scholar
11. Padfield, G.D. A theoretical model for helicopter flight mechanics for application to piloted simulation, Royal Aircraft Establishment, TR 81048, April 1981.Google Scholar