A Computer Program for Orbit Determination Using the Kalman Filter Approach

Author:

Mani Leelamma,Swaminathan V.

Publisher

Springer Netherlands

Reference9 articles.

1. Alan,M.K.: 1974, ‘Filtering theory methods and application to the orbit determination problem for near-earth satellites’, Ph.D. Thesis, Aerospace Studies, The University of Texas at Austin.

2. Escobal,P.R.: 1965, Methods of Orbit Determination,Wiley, N.Y.

3. Gunckel II,T.L.: 1966, ‘Guidance and Control of re-entry and aerospace vehicles’, Advances in Control Systems, 3, Acad. Press,N.Y.,pp.1–68.

4. Kalman,R.E.: 1961, ‘A new approach to linear filtering and prediction problems’, Trans.ASME J.Basic Engg. ,83, pp.95–107.

5. Leelamma Mani, P.V. Subba Rao,and V.Swaminathan: 1985, ‘KALIST — A Software for orbit determination’, Proceedings of the Workshop C4,- Seminar on Preliminary Orbit Determination, Indian Institute of Science, Bangalore.

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