Technical Papers
Oct 20, 2015

Take-Off and Landing Using Ground-Based Power-Simulation of Critical Landing Load Cases Using Multibody Dynamics

Publication: Journal of Aerospace Engineering
Volume 29, Issue 3

Abstract

A novel take-off and landing system using ground-based power is proposed in the EU-FP7 project GABRIEL. The main feature of this system is the complete removal of the landing gear from civil aircraft. The proposed system has the potential to reduce aircraft weight, emissions, and noise. A feasibility study of the structural design of the connection mechanism between aircraft and ground system has been performed by simulating the landing procedure on a moving ground system. One of the key challenges is the landing on a moving ground system under high crosswind conditions. The main focus in the current research is the calculation of the critical dynamic loads on both aircraft and ground system for a wide range of landing conditions (sink rate, velocity differences between aircraft and ground system, etc.). For comparison, conventional landing procedures with a traditional landing (TL) gear have also been simulated. The aerodynamics of the aircraft is represented by an accurate empirical model. The results of the simulations are a set of load cases and operational constraints that can be used for the structural design of the ground system and modifications to the aircraft. Eight critical load cases (combinations of vertical sink rate, horizontal velocity difference, and crosswind) are identified. These can be used instead of the traditional landing load cases specified in the certification specifications.

Get full access to this article

View all available purchase options and get full access to this article.

Acknowledgments

The authors would like to express their gratitude and thanks to Prof. Egbert Torenbeek for his valuable input related to the field of aircraft design. The authors are also grateful to Roy Bouma and Thomas Dumoulin who worked on the design of the connection mechanisms and helped with the development of the aerodynamic models.

References

AIRBUS. (2001). “Airbus industrie airbus A320-111 F-WWBA.” 〈http://www.airlinersillustrated.com/Airbus_Industrie_Airbus_A320111_FWWBA/p1737690_8074109.aspx〉 (Nov. 1, 2014).
Anonymous. (1979). The Usaf stability and control Datcom, Vol. I, McDonnell Douglas Astronautics Company, St. Louis.
Anonymous. (2000). “FSF ALAR briefing note 6.4-bounce recovery rejected landing.” Flight Safety Foundation, Alexandria, VA.
Anonymous. (2003). “Certification specifications for large aeroplanes (CS-25).”, European Aviation Safety Agency (EASA), Cologne, Germany.
Anonymous. (2005). “Flight operations briefing notes—Landing techniques: Bounce recovery rejected landing.” AIRBUS Customer Services, France.
Anonymous. (2007). “Flight operations briefing notes—Landing techniques: Preventing tailstrike at landing.” AIRBUS Customer Services, France.
Anonymous. (2008). “Flight operations briefing notes: Landing techniques—Crosswind landings.” AIRBUS Customer Services, France.
Anonymous. (2009). “Study on optimization design technology for landing gear shock-absorbing system of large civil aircraft, in college of aeronautics and astronautics.” Nanjing Univ. of Aeronautics and Astronautics, Nanjing, P.R China.
Anonymous. (2010a). MF-Tyre/MF-Swift 6.1.2.1 help manual, Dutch name of Netherlands Organisation for Applied Scientific Research (TNO), Helmond, Netherlands.
Anonymous. (2011a). “Jane’s all the world’s aircraft.”, Jane’s All the World's Aircraft, South Englewood, CO.
Anonymous. (2011b). “Safety recommendation: In reply refer to: A-11-68 and -69.” National Transportation Safety Board, Washington, DC.
Anonymous. (2012). “Aircraft characteristics airport and maintenance planning.”, AIRBUS Customer Services, France.
Baarspul, M., and Mulder, J. A. (1993). “The synthesis of flight simulation models: DATCOM techniques versus flight test identification.” Delft Univ. of Technology, Delft, Netherlands.
Berry, P. (2000). “Sizing the landing gear in the conceptual design phase.” 2000 World Aviation Conf., San Diego.
Chartier, B., Tuohy, B., Retallack, J., and Tennant, S. (2006). “LANDING gear shock absorber.”, Univ. of Duisburg-Essen, Essen, Germany.
Chester, D. H. (2002). “Aircraft landing impact parametric study with emphasis on nose gear landing conditions.” J. Aircr., 39(3), 394–403.
Ebbatson, M., Harris, D., and Jarvis, S. (2007). “Crosswind landings in general aviation: A modified method of reporting wing information to the pilot.” Int. J. Aviat. Psychol., 17(4), 353–370.
Eeckels, C. B. H. (2012). Magnetic assisted take-off for commercial aircraft, in faculty of aerospace engineering, Delft Univ. of Technology, Delft, Netherlands.
Graaff, A. D. (2014). “Cost benefit analysis of the GABRIEL concept.” GABRIEL deliverable D5.6, GABRIEL.
Hinson, D. R. (1994). “National transportation safety board-safety recommendation: In reply refer to: A-94-118 through -121.” National Transportation Safety Board/Federal Aviation Administration, Washington, DC.
Ijff, J. (1972). “Analysis of dynamic aircraft landing loads, and a proposal for rational design landing load requirements.” Delft Univ. of Technology, Delft, Netherlands.
Jeef Bland, D. C. (2002). “Preventing HARD nosegear touchdowns.” Boeing Commercial Airplanes, Seattle.
Khapane, P. D. (2004). “Simulation of aircraft landing gear dynamics using flexible multibody dynamics methods in Simpack.” 24th Congress of Int. Council of the Aeronautical Sciences, International Council of the Aeronautical Sciences (ICAS), Bonn, Germany.
Le Ngoc, L., Borst, C., Mulder, M., and van Paassen, M. M. (2010). “The effect of synthetic vision enhancements on landing flare performance.” AIAA GuidanceNavigation, and Control Conf., AIAA, Toronto.
MATLAB [Computer software]. MathWorks, Natick, MA.
Melin, T. (2001). User’s guide for Tornado 1.0, Royal Institute of Technology (KTH), Stockholm, Sweden.
Mori, R., and Suzuki, S. (2009a). “Analysis of pilot landing control in crosswind using neural networks.” Aerospace Conf., IEEE, New York, 1–10.
Mori, R., and Suzuki, S. (2009b). “Neural network modeling of lateral pilot landing control.” J. Aircr., 46(5), 1721–1726.
Pacejka, H. B., and Bakker, E. (1992). “The magic formula tyre model.” Veh. Syst. Dyn. Int. J. Veh. Mech. Mobility, 21(S1), 1–18.
Pacejka, H. B., and Besselink, I. J. M. (1997). “Magic formula tyre model with transient properties.” Veh. Syst. Dyn. Int. J. Veh. Mech. Mobility, 27(S1), 234–249.
Patterson, D., et al. (2002). “Design and simulation of an electromagnetic aircraft launch system.” IEEE Industry Applications Conf., Vol. 1–4, IEEE, Piscataway, NJ, 1950–1957.
Pfeiffer, T., et al. (2011). “Implementation of a heterogeneous, variable-fidelity framework for flight mechanics analysis in preliminary aircraft design.” Proc., 60. Deutscher Luft- und Raumfahrtkongress, German Society for Aeronautics and Astronautics (DGLR), Bonn, Germany.
Pool, D., et al. (2013). “Simulation technology and simulation of the GABRIEL concept.”, Delft Univ. of Technology (TUD), Delft, Netherlands.
Qi Pi, Q., Shi Wei, Q., Qi Zhi, M., and Shi Qing, Q. (2002). “Wing lift simulation in landing-gear drop test.” Mech. Sci. Technol., S1, 36–37.
Robert Majka, A. (2013). “Take-off aided by magnetic levitation technology.” Aircr. Eng. Aerosp. Technol., 85(6), 435–442.
Rogg, D., et al. (2012). “Preliminary specification of the ground based and on board sub-systems of the GABRIEL-system.”, GABRIEL.
Rogg, D., et al. (2013). “Conceptual design of the ground based system related to the GABRIEL concept.”, GABRIEL.
Rohacs, D., Voskuijl, M., and Siepenkötter, N. (2014). “Evaluation of landing characteristics achieved by simulations and flight tests on a small-scaled model related to magnetically levitated advanced take-off and landing operations.” 29th Congress of the Int. Council of the Aeronautical Sciences, International Council of the Aeronautical Sciences (ICAS), Bonn, Germany.
Rohacs, J., et al. (2012). “Possible solutions to take-off and land an aircraft.”, REA-TECH, Hungary.
Rohacs, J., and Rohacs, D. (2014). “The potential application method of magnetic levitation technology as a ground-based power to assist the aircraft takeoff and landing processes.” Aircr. Eng. Aerosp. Technol., 86(3), 188–197.
Roskam, J. (1985). Airplane design PART VI: Preliminary calculation of aerodynamic, thrust and power characteristics, Roskam Aviation and Engineering, Ottawa, KS.
Schmeitz, A. J. C., Besselink, I. J. M., and Jansen, S. T. H. (2007). “TNO MF-SWIFT.” Veh. Syst. Dyn. Int. J. Veh. Mech. Mobility, 45(S1), 121–137.
Schmollgruber, P., et al. (2013). “Conceptual design of the aircraft and aircraft systems using the GABRIEL concept.”, Office National d'Etudes et de Recherches Aérospatiales (ONERA), France.
Siepenkötter, N., et al. (2013). “Theoretical investigations deliverable D3.7: Conceptual design of the control system for using the GABRIEL concept.” Rheinisch-Westfälische Technische Hochschule Aachen Univ., Germany.
Spieck, M. (2004). “Simulation of aircraft landing impact under consideration of aerodynamic forces on the flexible structure.” 10th AIAA/ISSMO Multidisciplinary Analysis and Optimization Conf., American Institute of Aeronautics and Astronautics, Reston, VA.
Taylor, J. (1965). Manual on aircraft loads, Pergamon, Oxford.
Uhemeister, B. (2000). “Optimization of the passive shock absorber of a military aircraft.” RTO AVT Symp. on Active Control Technology for Enhanced Performance Operational Capabilities of Military Aircraft, Land Vehicles and Sea Vehicles,NATO Research and Technology Organisation (RTO), France.
Vos, R., et al. (2013). “Conceptual design of a magnetic-assisted take-off system for mid-range transport aircraft.” 51st AIAA Aerospace Sciences Meeting including the New Horizons Forum and Aerospace Exposition, AIAA, Dallas.
Vos, R., et al. (2014). “Analysis of a ground-based magnetic propulsion system.” J. Aircr., 51(3), 1013–1022.
Voskuijl, M., et al. (2012). “Preliminary evaluation of the environmental impact related to aircraft take-off and landings supported with ground-based (MAGLEV) power.” Air Transport and Operations Symp., Faculty of Aerospace Engineering, Delft, Netherlands.
Voskuijl, M., Klerk, J. D., and Ginneken, D. V. (2012). “Flight mechanics modelling of the Prandtl plane for conceptual and preliminary design.” Variational analysis and aerospace engineering: Mathematical challenges for aerospace design, Springer, London.
Voskuijl, M., Rocca, G. L., and Dircken, F. (2008). “Controllability of blended wing body aircraft.” 26th Int. Congress of the Aeronautical SciencesAnchorage, International Council of the Aeronautical Sciences (ICAS), Germany.
Westfall, J. R., Milwitzky, B., Silsby, N. S., and Dreher, R. C. (1957). “A summary of ground-loads statistics.” Langley Aeronautical Laboratory, National Advisory Committee for Aeronautics (NACA), Hampton, VA.
Wood, G., Blundell, M., and Sharma, S. (2012). “A low parameter tyre model for aircraft ground dynamic simulation.” Mater. Des., 35, 820–832.
Xu, K. (2012). “A novel dual fuzzy neural network to civil aviation aircraft disturbance landing control.” Commun. Comput. Inform. Sci., 289, 131–139.

Information & Authors

Information

Published In

Go to Journal of Aerospace Engineering
Journal of Aerospace Engineering
Volume 29Issue 3May 2016

History

Received: Dec 10, 2014
Accepted: May 1, 2015
Published online: Oct 20, 2015
Discussion open until: Mar 20, 2016
Published in print: May 1, 2016

Permissions

Request permissions for this article.

Notes

Part of the work in this paper has been presented in Wu, P., V. Mark, and J.L.V.T. Michael, Take-off and landing using ground based power-landing simulations using multibody dynamics, in 52nd Aerospace Sciences Meeting. 2014, American Institute of Aeronautics and Astronautics.

Authors

Affiliations

Ph.D. Candidate, Faculty of Aerospace Engineering, Delft Univ. of Technology, 2629 HS Delft, Netherlands (corresponding author). E-mail: [email protected]
M. Voskuijl
Assistant Professor, Faculty of Aerospace Engineering, Delft Univ. of Technology, 2629 HS Delft, Netherlands.
M. J. L. van Tooren
Professor of Aerospace Systems Design and Structures, Dept. of Mechanical Engineering, College of Engineering and Computing, Ronald E. McNAIR Center for Aerospace Innovation and Research, Univ. of South Carolina, 1000 Catawba St., Columbia, SC 29201.
L. L. M. Veldhuis
Professor, Faculty of Aerospace Engineering, Delft Univ. of Technology, 2629 HS Delft, Netherlands.

Metrics & Citations

Metrics

Citations

Download citation

If you have the appropriate software installed, you can download article citation data to the citation manager of your choice. Simply select your manager software from the list below and click Download.

Cited by

View Options

Get Access

Access content

Please select your options to get access

Log in/Register Log in via your institution (Shibboleth)
ASCE Members: Please log in to see member pricing

Purchase

Save for later Information on ASCE Library Cards
ASCE Library Cards let you download journal articles, proceedings papers, and available book chapters across the entire ASCE Library platform. ASCE Library Cards remain active for 24 months or until all downloads are used. Note: This content will be debited as one download at time of checkout.

Terms of Use: ASCE Library Cards are for individual, personal use only. Reselling, republishing, or forwarding the materials to libraries or reading rooms is prohibited.
ASCE Library Card (5 downloads)
$105.00
Add to cart
ASCE Library Card (20 downloads)
$280.00
Add to cart
Buy Single Article
$35.00
Add to cart

Get Access

Access content

Please select your options to get access

Log in/Register Log in via your institution (Shibboleth)
ASCE Members: Please log in to see member pricing

Purchase

Save for later Information on ASCE Library Cards
ASCE Library Cards let you download journal articles, proceedings papers, and available book chapters across the entire ASCE Library platform. ASCE Library Cards remain active for 24 months or until all downloads are used. Note: This content will be debited as one download at time of checkout.

Terms of Use: ASCE Library Cards are for individual, personal use only. Reselling, republishing, or forwarding the materials to libraries or reading rooms is prohibited.
ASCE Library Card (5 downloads)
$105.00
Add to cart
ASCE Library Card (20 downloads)
$280.00
Add to cart
Buy Single Article
$35.00
Add to cart

Media

Figures

Other

Tables

Share

Share

Copy the content Link

Share with email

Email a colleague

Share