Evaluation of the Modified Picard-Chebyshev Method for High-Precision Orbit Propagation

Author:

Koblick Darin1,Shankar Praveen2

Affiliation:

1. Graduate Student, Dept. of Mechanical and Aerospace Engineering, California State Univ. Long Beach, 1250 N. Bellflower Blvd., Long Beach, CA 90840.

2. Assistant Professor, Dept. of Mechanical and Aerospace Engineering, California State Univ. Long Beach, 1250 N. Bellflower Blvd., Long Beach, CA 90840 (corresponding author).

Publisher

American Society of Civil Engineers (ASCE)

Subject

Mechanical Engineering,Aerospace Engineering,General Materials Science,Civil and Structural Engineering

Reference40 articles.

1. American Institute of Aeronautics and Astronautics (AIAA). (2010). AIAA propagation specifications test cases and recommended practices Reston VA.

2. Orbit and uncertainty propagation: a comparison of Gauss–Legendre-, Dormand–Prince-, and Chebyshev–Picard-based approaches

3. Aristoff J. and Poore A. (2012). “Implicit Runge-Kutta methods for orbit propagation.” AAS/AIAA Astrodynamics Specialist Conf. American Institute of Aeronautics and Astronautics Reston VA.

4. Bai X. (2010). “Modified Chebyshev-Picard iteration methods for solution of initial value and boundary value problems.” Ph.D. thesis Texas A&M Univ. College Station TX.

5. Modified Chebyshev-Picard Iteration Methods for Orbit Propagation

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