Abstract
The solution of the spacecraft orbit determination problem is highly dependent upon the type of tracking data available at the ground station. Many algorithms exist for different types and combinations of tracking data. Well-funded tracking stations are typically able to supply six or more observed parameters simultaneously, enabling explicit solution of the orbit determination problem. The low-cost ground station under development at San José State University will initially be able to measure only Doppler shift as a function of time, thereby providing slant range rate as the single observable parameter. An algorithm enabling explicit solution of the orbit determination problem using range rate exclusively was not found, but orbit estimate improvement is still possible via differential correction. By utilizing a differential correction scheme in conjunction with a batch least squares estimator along with convergence improvements, the task of maintaining an acceptably accurate knowledge of the spacecraft orbit is made possible for a single ground station receiving a single measured parameter, even at higher levels of measurement noise and bias than those expected at the ground station.
Similar content being viewed by others
References
ESCOBAL, P. R. Methods of Orbit Determination, Kreiger Publishing Company, Malabar, FL, 1976 (reprint with corrections).
DANBY, J. M. A. Fundamentals of Celestial Mechanics, Willmann-Bell, Richmond, VA, 1992.
WERTZ, J. R. (editor) Spacecraft Attitude Determination and Control, D. Reidel Publishing Company, Dordecht, Holland, 1995.
BATE, R. R, MUELLER, D. D., and WHITE, J. E. Fundamentals of Astrodynamics, Dover Publications, Inc, New York, 1971.
PRUSSING, J. and CONWAY, B. Orbital Mechanics, Oxford University Press, Inc., New York, NY, 1993.
PATTON, R. B., JR. “Orbit Determination from Single Pass Doppler Observations,” Institute of Radio Engineers Transactions on Military Electronics, Vol. 4, Nos. 2 and 3, April–July 1960, pp. 336–9.
REICHERT, A., AXELRAD, P., WU, S. C., BERTIGER, W., and SRINIVASAN, J. “Initial Demonstration of a Point Solution Algorithm for Orbit Determination Using the microGPS Receiver,” Proceedings of the ION National Technical Meeting, 1997.
The Astronautical Almanac, 1994, U.S. Government Printing Office, Washington, D.C., 1994.
WEEKS, C. J., BUXCHELMAN, A., and SABILLO, R. “Direct Determination of a Spacecraft Orbit From the Doppler Data Signature,” The Journal of the Astronautical Sciences, Vol. 47, Nos. 3 and 4, July–December 1999, pp. 295–9.
Author information
Authors and Affiliations
Rights and permissions
About this article
Cite this article
Coyle, D., Pernicka, H.J. Orbit Determination at a Single Ground Station Using Range Rate Data. J of Astronaut Sci 49, 327–344 (2001). https://doi.org/10.1007/BF03546325
Published:
Issue Date:
DOI: https://doi.org/10.1007/BF03546325