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Dynamics and control of a high-altitude balloon with slung load

Published online by Cambridge University Press:  31 October 2024

L. Chen*
Affiliation:
School of Air Transportation, Shanghai University of Engineering Science, Shanghai, China
Z. Song
Affiliation:
School of Air Transportation, Shanghai University of Engineering Science, Shanghai, China
J. Lin
Affiliation:
School of Air Transportation, Shanghai University of Engineering Science, Shanghai, China
*
Corresponding author: L. Chen; Email: [email protected]

Abstract

The high-altitude balloon proposed in this paper is a long-life balloon carrying a payload through a cable that flies at 20km altitude in near space. A dynamic model of the system, including the thermodynamics of the buoyancy body coupled with a hanging model of the pod, is developed using the Newton–Euler method. The buoyancy body consists of a helium balloon and a ballonet. A differential pressure difference-based altitude adjustment is achieved by tracking the pressure difference at the target altitude. A dynamic simulation of the buoyancy body with a slung pod in autonomous vertical takeoff and altitude regulation processes is presented. The internal thermodynamic variations and pressure differential of the buoyancy body are given. The air mass exchange and blower flow control of the ballonet are validated. The altitude holding error is analysed. The maximum pull force that the cable can withstand is calculated, and the maximum attitude angles of the pod during the ascending and descending processes are depicted. Simulation results provide basic knowledge for the structural design and payload installation of pods.

Type
Research Article
Copyright
© The Author(s), 2024. Published by Cambridge University Press on behalf of Royal Aeronautical Society

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References

d’ Oliveira, F.A., Francisco, C.L. and Tessaleno, C.D. High-altitude platforms present situation and technology trends, J. Aerospace Technol. Manag., 2016, 8, (3), pp 249262.Google Scholar
Andurkar, A.G. and PrachiZodpe. A review paper on project “LOONS”, Int. J. Adv. Res. Comput. Commun. Eng., 2016, 5, (3), pp 132138.Google Scholar
Oktay, T. and Sultan, C. Modeling and control of a helicopter slung-load system, Aerospace Sci. Technol., 2013, 29, pp 206222 CrossRefGoogle Scholar
Pankine, A., Li, Z.Q. and Parsons, D. Stratospheric satellites for earth observations, American Meteorological Society, August 2009, DOI: 10.1175/2009BAMS2624.1 CrossRefGoogle Scholar
Zaugg, E.C., Margulis, A., et al. SAR imaging from stratospheric balloons: first results, 2019 IEEE Radar Conference, DOI: 10.1109/RADAR.2019.8835692 CrossRefGoogle Scholar
Sadr, S., Moosavian, A.A. and Zarafshan, P. Dynamics modeling and control of a quadrotor with swing load, J. Rob., 2014, Article ID 265897, 12 pp.CrossRefGoogle Scholar
Hoh, R.H., Heffley, R.K. and Mitchell, D.G. Development of Handling Qualities Criteria for Rotorcraft with Externally Slung Loads, NASA/CR-2006-213488, U.S. Army RDECOM No. AFDD/TR-06-003.Google Scholar
Stuckey, R.A. Mathematical modelling of helicopter slung-load systems: DSTO-TR-1257 [R]. US, 2001.Google Scholar
Pal, R.S. Modelling of helicopter underslung dynamics using Kane’s method, IFAC Papers On Line, 2020, 53, (1), pp 536542.CrossRefGoogle Scholar
Weber, J.M. and Greif, R.K. A Lagrange-D’Alembert formulation of the equations of motion of a helicopter carrying an externally suspended load, NASA Technical Memorandum 85864, 1985Google Scholar
Ardema, M.D. Vehicle Concepts and Technology Requirements for Buoyant Heavy-Lift Systems, NASA Technical Paper, 1921, pp 1–19Google Scholar
Abdallah, F.B., Hima, S., Azouz, N., Beji, L. and Abichou, A. Modeling and control of an airship-mounted crane for freight transportation, IFAC Papers Line, 2018, 51, (9), pp 452457.CrossRefGoogle Scholar
Abdallah, F.B., Azouz, N., Beji, L. and Abichou, A.  Modeling of a heavy-lift airship carrying a payload by a cable-driven parallel manipulator, Int. J. Adv. Rob. Syst., 2019, 16, (4), pp 117. Google Scholar
Bugga, R., Jones, J.P. and Pauken, M. Extended-range variable altitude balloons for venus atmospheric missions, Acta Astronautica, 2022, 197, pp 6980.CrossRefGoogle Scholar
Vandermeulen, I., Guay, M. and Mclellan, P.J. Formation control of high-altitude balloons by distributed extremum seeking control, American Control Conference, IEEE, 2016, Boston, pp 25242529.CrossRefGoogle Scholar
Borges, A., Battistini, S., Cappelletti, C. and Honda, Y.M. Altitude control of a remote-sensing balloon platform, Aerospace Sci. Technol., 2021, 110, p 106500.CrossRefGoogle Scholar
Saleh, S. and He, W.L. Ascending performance analysis for high altitude zero pressure balloon, Adv. Space Res., 2017, 59, pp 21582172.CrossRefGoogle Scholar
Öznur, K.M. and Alaittin, H. Modeling of stratospheric balloon using transport phenomena and gas compress–release system, J. Thermophys. Heat Transfer, 2014, 28, (3), pp 534541.CrossRefGoogle Scholar
Shi, H., Song, B.Y., and Yao, Q.P. Thermal performance of stratospheric airships during ascent and descent, J. Thermophys. Heat Transfer, 2009, 23, (4), pp 816821.CrossRefGoogle Scholar
Carlson, L.A. and Horn, W.J. New thermal and trajectory model for high-altitude balloons, AIAA J. Aircraft, 1983, 20, (6), pp 500507.CrossRefGoogle Scholar
Schallenkamp, R.S., Siewert, A.D. and Lachenmeier, T.T. Parametric analysis Of Overpressure Zero Pressure (OZP) balloons using the SINBAD computer model, 32nd Aerospace Sciences Meeting & Exhibit, January 10-13, 1994/ Reno, NV AIAA 94-0515.CrossRefGoogle Scholar