Skip to main content

Navigation Analysis

  • Chapter
  • First Online:
Book cover Planetary Spacecraft Navigation

Part of the book series: Space Technology Library ((SPTL,volume 37))

  • 1529 Accesses

Abstract

Navigation analysis is performed to aid mission design and to verify the veracity of the navigation system. The latter can be separated into three time ordered phases being pre-flight, during mission operations and post-flight. Pre-flight analysis is probably the most important. It involves imagining problems that the navigation system could have during flight and determining the performance of the proposed navigation system. These problems are resolved and the spacecraft and navigation system design can be modified as appropriate. After launch, it is too late to alter the spacecraft design. During mission operations the spacecraft is generally in the cruise mode for long periods of time. Navigation analysis continues as before launch with an emphasis on navigation operations. There is not much interest in discovering during cruise that the spacecraft design cannot achieve mission success. Another source of problems arise from unexpected performance of the navigation system. These problems can be mission catastrophic. However, sometimes there is enough time to solve the problem and salvage the mission. This generally only happens if the problem is simple to solve. During mission operations, a computer solution that takes a week to implement will probably be too late. Post-flight analysis could be useful for problems that may arise during future mission operations. However, funds are generally not available if the mission was determined to be a success.

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

Access this chapter

Chapter
USD 29.95
Price excludes VAT (USA)
  • Available as PDF
  • Read on any device
  • Instant download
  • Own it forever
eBook
USD 79.99
Price excludes VAT (USA)
  • Available as EPUB and PDF
  • Read on any device
  • Instant download
  • Own it forever
Softcover Book
USD 99.99
Price excludes VAT (USA)
  • Compact, lightweight edition
  • Dispatched in 3 to 5 business days
  • Free shipping worldwide - see info
Hardcover Book
USD 109.99
Price excludes VAT (USA)
  • Durable hardcover edition
  • Dispatched in 3 to 5 business days
  • Free shipping worldwide - see info

Tax calculation will be finalised at checkout

Purchases are for personal use only

Institutional subscriptions

Bibliography

  1. Bursa, M., Z. Martinec, K. Pec 1990. Principal Moments of Inertia, Secular Love Number and Origin of Phobos. Adv. Space Res. Vol 10, No 3–4, pp.(3)67–(3)70.

    Google Scholar 

  2. Capen, E. B. and A. E. Joseph, “Software Requirements Document Viking Project - MOIOP”, JPL Report, 1973.

    Google Scholar 

  3. Dunham, D. W., McAdams, 1. V., Mosher, L. E. and Helfrich, C. E., “Maneuver Strategy for NEAR’s Rendezvous with 433 Eros”, Paper IAF-97-A.4.01 presented at the 48th International Astronautical Federation Congress, Turin, Italy, Oct. 6–10,1997.

    Google Scholar 

  4. Dunham, D. W., et al, 1999. Recovery of NEARs Mission to Eros. International Astronautical Congress Paper IAF-99-Q.5.05, Amsterdam, The Netherlands.

    Google Scholar 

  5. Duxbury, T. C. 1989. The Figure of Phobos.Icarus 78, 169–180.

    Google Scholar 

  6. Farquhar, R. W., ed., 1995. Special Issue on theNear Earth Asteroid Rendezvous Mission. J. Astronaut. Sci. 43.

    Google Scholar 

  7. Farquhar, R. W., Dunham, D. W. and McAdams,1. V., “NEAR Mission Overview and Trajectory Design,” J Astron. Sciences, Vol. 43, No.4, Oct.-Dec. 1995, pp. 353–371.

    Google Scholar 

  8. Guo, Y., R. W. Farquhar, “New Horizons Mission Design for the Pluto-Kuiper Belt Mission”, AIAA paper 2002–4722, AIAA/AAS Astrodynamics Specialist Conference, Monterey, California, August 5–8, 2002.

    Google Scholar 

  9. Guo, Y., R. W. Farquhar, “New Horizons Pluto-Kuiper Belt Mission: Design and Simulation of the Pluto-Charon Encounter”, IAC paper 02-Q.2.07, 53rd International Astronautical Congress The World Space Congress-2002, Houston, Texas, October 5–8, 2002.

    Google Scholar 

  10. Guo, Y., R. W. Farquhar, “New Horizons Mission Design for the Pluto-Kuiper Belt Mission”, AIAA paper 2002–4722, AIAA/AAS Astrodynamics Specialist Conference, Monterey, California, August 5–8, 2002.

    Google Scholar 

  11. Guo, Y., R. W. Farquhar, “New Horizons Pluto-Kuiper Belt Mission: Design and Simulation of the Pluto-Charon Encounter”, IAC paper 02-Q.2.07, 53rd International Astronautical Congress The World Space Congress-2002, Houston, Texas, October 5–8, 2002.

    Google Scholar 

  12. Konopliv, A.S., W.B. Banerdt, and W.L. Sjogren 1999. Venus Gravity: 180th Degree and Order Model. Icarus 139, 3–18.

    Article  Google Scholar 

  13. Keating, G. M., J. Y. NicholsonIII, and L. R. Lake, “Venus Upper Atmosphere Structure”, Journal of Geophysical Research, vol. 85, no. A13, pp 7941–7956, December 30, 1980.

    Google Scholar 

  14. King-Hele, D., Theory of Satellite Orbits in an Atmosphere, Butterworths, London, 1964.

    MATH  Google Scholar 

  15. Kolyuka, Y. F., S. M. Kudryavtsev, V. P. Tarasov, V. F. Tikhonov, N. M. Ivanov, V. S. Polyakov, V. N. Potchukaev, O. V. Papkov, E. L. Akim, R. R. Nasirov 1990. Report of the International Project “Phobos” Experiment “Celestial Mechanics”, in press.

    Google Scholar 

  16. McAdams, 1. V., Dunham, D. W., Helfrich, C. E., Mosher, L. E. and Ray, 1. c., “Maneuver History of the NEAR Mission: Launch through Earth Swingby Phase,” Paper rSTS 98-c-23, 21st International Symposium on Space Technology and Science, Sonic City, Omiya Japan, May 24–31, 1998.

    Google Scholar 

  17. McAdams, J. V., D. W. Dunham, R. W. Farquar, T. H. Taylor, B. G. Williams, “Trajectory Design and Maneuver Strategy for the MESSENGER Mission to Mercury”, Paper 05–173, 15th AAS/AIAA Space Flight Mechanics Conference, Copper Mountain,CO, January 23–27, 2005.

    Google Scholar 

  18. Miller, J.K. and F. T. Nicholson, “Galileo Jupiter Approach Orbit Determination”, The Journal of the Astronautical Sciences, Vol 32, No 1, January-March, 1984, pp 63–79.

    Google Scholar 

  19. Miller, J. K., Weeks, C. J. and Wood, L. J., “Orbit Determination Strategy and Accuracy for a Comet Rendezvous Mission,” J Guidance, Control, and Dynamics, Vol. 13, No.5, Sep.-Oct. 1990., pp. 775–784.

    Article  Google Scholar 

  20. Miller, J. K., Williams, B. G., Bollman, W. E., Davis, R. P., Helfrich, C. E., Scheeres, D. 1., Synnott, S. P., Wang, T. C. and Yeomans, D. K., “Navigation Analysis for Eros Rendezvous and Orbital Phases,” J Astron. Sciences, Vol. 43, No.4, Oct.-Dec. 1995, pp. 453–476.

    Google Scholar 

  21. Miller, J. K., et. al., “Navigation Analysis for Eros Rendezvous and Orbital Phases”, The Journal of the Astronautical Sciences, Vol 43, No 4, October-December 1995, pp 453–476

    Google Scholar 

  22. Miller, J. K., P. G. Antreasian, R. W. Gaskell, J. Giorgini, C. E. Helfrich, W. M. Owen, B. G. Williams and D. K. Yeomans, Determimation of Eros Physical Parameters for NEAR Earth Asteroid RendezvousOrbit Phase Navigation. AAS paper 99–463, AAS/AIAA Astrodynamics Specialist Conference, Girdwood, Alaska., 1999

    Google Scholar 

  23. Miller, J. K., P. G. Antreasian, J. J. Bordi, S. Chesley, C. E. Helfrich, A. Konopliv, W. M. Owen, T. C. Wang, B. G. Williams and D. K. Yeomans, Determination of Eros Physical Parameters from Near Earth Asteroid Rendezvous Orbit Phase Navigation Data. AIAA paper 2000–4422, AAS/AIAA Astrodynamics Specialist Conference, Denver, Colorado, 2000.

    Google Scholar 

  24. Miller, J. K. et alia, ”Determination of the Shape, Gravity and Rotational State 0f Asteroid 433 Eros“, Icarus, Vol. 155 Number 1, pp. 3–17, January 2002.

    Google Scholar 

  25. Miller, L. J., J. K. Miller and W. E. Kirhofer, “Navigation of the Galileo Mission,” Paper 83–1002, presented at the AIAA 21 st Aero- space Science Meeting, Reno, Nevada, January 1983.

    Google Scholar 

  26. Mottinger, N. A., “DSN Coverage Requirements for PVO Reentry”, IOM 314.7–165, 5 February 1992

    Google Scholar 

  27. O’Neil, W. J., and R. T. Mitchell, “Galileo Mission Overview,” Paper 83–0096, presented at the AIAA 21st Aerospace Science Meeting, Reno, Nevada, January, 1983.

    Google Scholar 

  28. Peale, S. J. 1977. Rotational histories of the natural satellites. In Planetary Satellites (J. Burns, Ed), pp. 87–112. Univ. of Arizona Press, Tucson.

    Google Scholar 

  29. Rourke, K. H., “Navigation of the 1982 Jupiter Orbiter-Probe Mission, ” paper presented at the AAS/AIAA Astrodynamics Specialists Conference, Jackson Hole, Wyoming, September, 1977.

    Google Scholar 

  30. Ryne, M. S., N. A. Mottinger, P. R. Menon, J. K. Miller, “Navigation of Pioneer 12 During Atmospheric Reentry at Venus”, AAS 93–712, AAS/AIAA Astrodynamics Specialist Conference, Victoria, B.C., Canada, August 16, 1993.

    Google Scholar 

  31. Russell, R. K., “The Effect of Atmospheric Drag on Position and Velocity Errors of Orbiting Spacecraft”, JPL

    Google Scholar 

  32. Russell, R. K., “Gravity Focussing of Hyperbolic Trajectories,” Technical Memorandum 391–424, Jet Propulsion Laboratory internal document, Pasadena, California, 30 March 1973.

    Google Scholar 

  33. Scheeres, D. J., “Analysis of Orbital Motion Around 433 Eros,” 1. Astron. Sciences, Vol. 43, No.4, Oct.-Dec. 1995, pp. 427–452.

    MathSciNet  Google Scholar 

  34. Thomas, P. C. et alia, “Eros: Shape, Topography, and Slope Processes”, Icarus, Vol. 155 No 1, pp 18–37, January 2002.

    Google Scholar 

  35. Vojvodich, N. S., et al., Galileo Atmospheric Entry Probe Mission Description, Paper 83–0100, presented at the AIAA 21st Aerospace Science Meeting, Reno, Nevada, January, 1983.

    Google Scholar 

Download references

Author information

Authors and Affiliations

Authors

Rights and permissions

Reprints and permissions

Copyright information

© 2019 Springer International Publishing AG, part of Springer Nature

About this chapter

Check for updates. Verify currency and authenticity via CrossMark

Cite this chapter

Miller, J. (2019). Navigation Analysis. In: Planetary Spacecraft Navigation. Space Technology Library, vol 37. Springer, Cham. https://doi.org/10.1007/978-3-319-78916-3_9

Download citation

  • DOI: https://doi.org/10.1007/978-3-319-78916-3_9

  • Published:

  • Publisher Name: Springer, Cham

  • Print ISBN: 978-3-319-78915-6

  • Online ISBN: 978-3-319-78916-3

  • eBook Packages: EngineeringEngineering (R0)

Publish with us

Policies and ethics