Integrated Model for Prediction of Reentry Time of Risk Objects-Reference-Cited by-同舟云学术

Integrated Model for Prediction of Reentry Time of Risk Objects

Published:2015-01 Issue:1 Volume:52 Page:295-299
ISSN:0022-4650
Container-title:Journal of Spacecraft and Rockets
language:en
Short-container-title:Journal of Spacecraft and Rockets

Author:

Gupta Shraddha¹,Anilkumar A. K.¹

Affiliation:

1. Applied Mathematics Division, Indian Space Research Organisation, Vikram Sarabhai Space Center, Kerala 695 022, India

Publisher

American Institute of Aeronautics and Astronautics (AIAA)

Subject

Space and Planetary Science,Aerospace Engineering

Link

https://arc.aiaa.org/doi/pdf/10.2514/1.A32704

Reference10 articles.

1. JohnsonN. L.McKnightD. S., Artificial Space Debris, Orbit, Malabar, FL, 1987, pp. 1–9.

2. King-HeleD., Satellite Orbits in an Atmosphere: Theory and Applications, Springer–Verlag, London, 1987, pp. 25–65.

3. StrizziJ. D. “Improved Algorithm for Satellite Orbit Decay and Re-Entry Prediction,” M.S. Thesis, Dept. of Aeronautics and Astronautics, Massachusetts Inst. of Technology, Cambridge, MA, June 1993.

4. A constant gain Kalman filter approach for the prediction of re-entry of risk objects

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