Velocity-space maps and transforms of tracking observations for orbital trajectory state analysis

Author:

Altman Samuel P.

Publisher

Springer Science and Business Media LLC

Subject

Space and Planetary Science,Astronomy and Astrophysics,Applied Mathematics,Computational Mathematics,Mathematical Physics,Modelling and Simulation,General Medicine

Reference13 articles.

1. Altman, S. P. and Pistiner, J. S.: 1968, ‘Application of State Space Transformation Theory to Orbit Determination and Prediction’, AAS Paper No. 68-111, AAS/AIAA Astrodynamics Specialist Conference, Jackson, Wyoming, September 3–5.

2. Altman, S. P. and Pistiner, J. S.: 1970, ‘A New Generating Principle for Two-Fixed Center Orbits: Conic Solutions’,Proceedings of the XIXth International Astronautical Congress, Vol. 2, Astrodynamics and Astrionics, Pergamon Press, pp. 27–57.

3. Altman, S. P.: 1972, ‘A Unified State Model of Orbital Trajectory and Attitude Dynamics’,Celes. Mech. 6, 425–446.

4. Hamilton, Sir William Rowan: 1866, in C. J. Joly (ed.),Elements of Quaternions, Volumes I and II. Reprint by Chelsea Publishing Co., New York 1969.

5. Halberstam, H. and Ingram, R. E. (eds): 1967,The Mathematical Papers of Sir William Rowan Hamilton, Vol. III: Algebra, Cambridge University Press.

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