State Transition Matrix for Perturbed Orbital Motion Using Modified Chebyshev Picard Iteration

Author:

Read Julie L.,Younes Ahmad Bani,Macomber Brent,Turner James,Junkins John L.

Publisher

Springer Science and Business Media LLC

Subject

Space and Planetary Science,Aerospace Engineering

Reference29 articles.

1. Bai, X., Junkins, J.L.: Modified Chebyhev-Picard iteration methods for orbit propagation. J. Astronaut. Sci. 58(4), 583–613 (2011)

2. Bai, X: Modified chebyshev-picard iteration methods for solution of initial value and boundary value problems. PhD Dissertation, Texas A&M University, College Station, TX (2010)

3. Woollands, R., Junkins, J.L.: A new solution for the General Lambert problem. In: Proceeding of 2015 AAS GN&C Conference, Breckenridge, CO (2014)

4. Macomber, B., Wollands, R., et al.: Modified Chebyshev Picard iteration for efficient numerical integration of ordinary differential equations. In: Proceeding of 2013 AAS GN&C Conference, Breckenridge, CO (2013)

5. Kim, D., Junkins, J.L.: Multi-segment adaptive modified Chebyshev Picard iteration method. In: Proceeding of 2014 AAS/AIAA Space Flight Mechanics Conference, Santa Fe, NM (2014)

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