Skip to main content
Log in

Planetary exploration by robotic aerovehicles

  • Published:
Autonomous Robots Aims and scope Submit manuscript

Abstract

Planetary aerobots are a new type of telerobotic science platform that can fly and navigate in a dynamic 3-dimensional atmospheric environment, thus enabling the global in situ exploration of planetary atmospheres and surfaces. Aerobots are enabled by a new concept in planetary balloon altitude control, developed at JPL, which employs reversible-fluid changes to permit repeated excursions in altitude. The essential physics and thermodynamics ofreversible-fluid altitude control have been demonstrated in a series of altitude-control experiments conducted in the Earth's atmosphere, which are described. Aerobot altitude-control technology will be important in the exploration of seven planets and satellites in our solar system. Three of these objects—Venus, Mars, and the Saturnian satellite Titan—have accessible solid surfaces and atmospheres dominated by the dense gases nitrogen or carbon dioxide. They will be explored with aerobots using helium or hydrogen as their primary means of buoyancy. The other four planets—Jupiter, Saturn, Uranus, and Neptune—have deep atmospheres that are predominantly hydrogen. It may be possible to explore these atmospheres with aerobots inflated with atmospheric gas that is then radiatively heated from the hotter gaseous depths below. To fulfill their potential, aerobots to explore the planets will need autonomous state estimators to guide their observations and provide information to the altitude-control systems. The techniques of acquiring these data remotely are outlined. Aerobots will also use on board altitude control and navigation systems to execute complex flight paths including descent to the surface and exploiting differential wind velocities to access different latitude belts. Approaches to control of these systems are examined. The application of aerobots to Venus exploration is explored in some detail: The most ambitious mission described, the Venus Flyer Robot (VFR), would have the capability to make repeated short excursions to the high-temperature surface environment of Venus to acquire data and then return to the Earth-like upper atmosphere to communicate and recool its electronic systems. Finally a Planetary Aerobot Testbed is discussed which will conduct Earth atmospheric flights to validate autonomous-state-estimator techniques and flight-path-control techniques needed for future planetary missions.

This is a preview of subscription content, log in via an institution to check access.

Access this article

Price excludes VAT (USA)
Tax calculation will be finalised during checkout.

Instant access to the full article PDF.

Similar content being viewed by others

References

  • Akiba, R., Hinada, M., and Nakajima, T. 1992. Simulation study of venus balloon system. Paper IAF-92-0559 presented at the 43rd Congress of the International Astronautical Federation.

  • Anderson, C.M. 1991. Wind, Sand and Mars: The 1990 Tests of the Mars balloon and snake.The Planetary Report, 11(1):12–15.

    Google Scholar 

  • Biregovoy, S.N. 1993. The hopping motion balloon station in the lower layers of the venusian atmosphere. Informal Technical Brief, Babakin Center, Moscow.

    Google Scholar 

  • Blamont, J. et al. 1993. Balloons on planet Venus: Final results.Proceedings on Scientific Ballooning. Adv. Space Res., Pergamon Press, 13(2):145–152.

    Google Scholar 

  • Blamont, J. 1981. Balloons on other planets.Adv. Space Res., 1:63–69.

    Google Scholar 

  • Blamont, J. 1993. Development of Mars network by balloons.Intl. Workshop for Coordination of Mars Exploration, Germany, CNES/DG/CN No. 1631, Paris.

  • Blamont, J. 1993. Balloons for the exploration of Mars.Adv. Space Res., 13(2):137–144.

    Google Scholar 

  • Blamont, J., Heinsheimer, T., and Pommerean, J.P. 1974. Nouvelle methode d'etude de la dynamique de la stratosphere; principe et premiers resultats. Academie des Sciences (Paris), Comptes Rendus, Seris B—Sciences Physiques, 278(7):249–254.

    Google Scholar 

  • Blamont, J.T. 1985. The exploration of the atmosphere of venus by balloons.Space Research. 5(9):99–106.

    Google Scholar 

  • Carlson, L.A. and Horn. W.J. 1983. New thermal and trajectory model for high-altitude balloons.AIAA Journal of Aircraft, 20:500–507.

    Google Scholar 

  • Crisp, D., Cozman, and Krotkov, E. 1990. Vega balloon meteorological measurements.Adv. Space Res., 10(5):109–124.

    Google Scholar 

  • Cutts, J.A., Nock, K.T., Jones, J.A., Rodriguez, G., Balaram, J., Powell, G.E., and Synnott, S.P. 1995. New means for mobility.IEEE Conference on Robotics & Automation, Nagoya, Japan.

  • Desjean, M.C. 1981. A balloon and its basket in the Venus atmosphere. InProceedings of the 2nd Int'l Conf. Numerical Methods in Thermal Problems, 2:1302-1313, Italy.

  • DiCicco, A., Nock, K.T., and Powell, G.E. 1995. Balloon experiment at Venus (BEV). InProceedings 11th Lighter-Than-Air Technology Conference, AIAA 95-1623, Clearwater, FL.

  • Gildenberg, B.D. 1970. General philosophy and techniques of balloon control.6th AFCRL Scientific Balloon Symposium.

  • Houghton, J.T. 1977.The Physics of Atmospheres, Cambridge University Press, p. 203.

  • Hunter, D.M., Colin, L. Donahue, T., and Moroz, V. 1983.Venus, The University of Arizona Press.

  • Jones, Jack A. 1995. Reversible fluid balloon altitude control concepts. InProceedings of the 11th Lighter-Than-Air Systems Technology Conference, AIAA-95-1621, Clearwater, FL.

  • Koshlyakov, V.N. 1984. The Magnus effect. DOP-UKR-A, 4:39–43.

    Google Scholar 

  • Krotkov, E., Hebert, M., and Simmons, R. 1996. Stereo perception and dead reckoning for a prototype lunar rover.Journal of Autonomous Robots, Special Issue on Autonomous Vehicles for Planetary Exploration.

  • Malaterre, P. 1993. Long duration balloon flights in the middle stratosphere.Adv. Space Res., 13(2):107–114.

    Google Scholar 

  • Matijevic, J. and Shirley, D. 1996. Mars pathfinder rover.Journal of Autonomous Robots, Special Issue on Autonomous Vehicles for Planetary Exploration.

  • Matthies, L., Gat, E., Harrison, R., Wilcox, B., Volpe, R., and Litwin, T. 1996. Mars microrover navigation: Performance evaluation and enhancement.Autonomous Robots, Special Issue on Autonomous Vehicles for Planetary Exploration.

  • Moroz, V.I., 1994. VA-94 Venus atmosphere model for discovery venera project. Space Research Institute of Russian Academy of Science (IKI), Profsojuznaja, 84/32, Moscow.

    Google Scholar 

  • Moskalenko, G.M. 1978.Mekhanika poleta v atmosfere venery, Mashinosteroenie Publishers, Moscow.

    Google Scholar 

  • Moskalenko, G.M. and Troshin, V.S. 1980. Izbytochnoye devleniye v aerostaticheskoy obolochke i vozmozhnost' ego regulirovaniya pri plavanii v atmosfere Venery. Excess Pressure in an Aerostatic Shell and the Possibility of its Regulation During Floating in the Atmosphere of Venus,Kosmicheskiye Issledovaniya, 18:474–476.

    Google Scholar 

  • Moskalenko, G.M. 1981. Dirizhabl' dlya Venery (Dirigibles for Venus),Nauka i Zhizn, 9:85–87.

    Google Scholar 

  • Needleman, H.C., Nock, R.S., and Bawcom, D.W. 1993. Status of the NASA balloon program.Adv. Space Res., 13(2):69–76.

    Google Scholar 

  • Nishimura, J., Yajima, N., Fujii, M., and Yokota, R. 1990. A model experiment of the Venus balloon. InProceedings of the International Symposium on Space Technology and Science, Tokyo,pp. 1589–1592.

  • Nock, K.T., Aaron, K.M., Jones, J.A., McGee, D.P., Powell, G.E., Yavrouian, A., and Wu, J.J. 1995. Balloon altitude control experiment (ALICE) project.Proceedings 11th Lighter-Than-Air Systems Technology Conference, AIAA-95-1632, Clearwater, FL.

  • Robertson, D.F. 1994. To boldly go: A new generation of rovers are poised to explore surfaces on the Moon, Venus, Mars and beyond.Astronomy, 22(12):.

  • Romero, M. 1980. Balloon sur Venus—Gonflage sous Parachute et Oscillations de Balloon Ludion (Balloons over Venus—Inflation under Parachute and Ludion Balloons Oscillations). Centre d'Etude et due Recherches de Toulouse, ONERA, CR/BAL/THER/49.

  • Romero, M. 1981. Balloon sur Venus—Simulations de Divers Modes de Stabilization (Balloons over Venus)—Simulations of Various Stabilization Methods). Convention 81/CNES/0728, Etude Cert 412, CR/BAL/THER 151.

  • Rougeron, M. 1969. CNES Article 329/DET/TO/BA/EE.

  • Schubert, G., 1983. General circulation and the dynamical state of the Venus atmosphere.Venus, The University of Arizona Press, Tucson, pp. 681–765

    Google Scholar 

  • Science, 1986. Special issue on venus ballooning.

  • Sirmain, C., Evard, J., and Vega, J. 1995. Martian aerostat deployment: Analysis and test paper. Presented at AIAA 11th Lighter-Than-Air Conference, Clearwater, FL.

  • Vorachek, J.J. 1970. A comparison of several very high altitude station keeping balloon concepts.6th AFCRL Balloon Symposium, pp. 355–381.

  • Wu, J.J. and Jones, J.A. 1995. Performance models for reversible fluid balloons. InProceedings 11th Lighter-Than-Air Technology Conference, AIAA-95-1623, Clearwater, FL.

  • Yavrouian, A., Plett, G., and Yen, S.S. 1995. High temperature balloon materials for Venus balloon envelopes. InProceedings of the 11th Lighter-Than- Air Systems Technology Conference, AIAA-95-1617, Clearwater, FL.

  • Zubrin, R., Price, S. Clark, B. Cantrell, J., and Bourke, R. 1993. A new Mars aerial platform.Aerospace America, pp. 20–24.

Download references

Author information

Authors and Affiliations

Authors

Rights and permissions

Reprints and permissions

About this article

Cite this article

Cutts, J.A., Nock, K.T., Jones, J.A. et al. Planetary exploration by robotic aerovehicles. Auton Robot 2, 261–282 (1995). https://doi.org/10.1007/BF00710794

Download citation

  • Issue Date:

  • DOI: https://doi.org/10.1007/BF00710794

Keywords

Navigation