Etienne Pellegrini
Etienne Pellegrini
Mission Design Engineer, NASA Jet Propulsion Laboratory
Verified email at jpl.nasa.gov - Homepage
Title
Cited by
Cited by
Year
F and G Taylor series solutions to the Stark and Kepler problems with Sundman transformations
E Pellegrini, RP Russell, V Vittaldev
Celestial Mechanics and Dynamical Astronomy 118 (4), 355-378, 2014
232014
On the Computation and Accuracy of Trajectory State Transition Matrices
E Pellegrini, RP Russell
Journal of Guidance, Control, and Dynamics 39 (11), 2485-2499, 2016
222016
A Multiple-Shooting Differential Dynamic Programming Algorithm
E Pellegrini, RP Russell
AAS/AIAA Space Flight Mechanics Meeting, 2017
162017
Tour Design Techniques for the Europa Clipper Mission
S Campagnola, BB Buffington, T Lam, AE Petropoulos, E Pellegrini
Journal of Guidance, Control, and Dynamics 42 (12), 2615-2626, 2019
92019
Quasi-Newton Differential Dynamic Programming for Robust Low-Thrust Optimization
E Pellegrini, RP Russell
AIAA/AAS Astrodynamics Specialists Conference, 2012
82012
Applications of the Multiple-Shooting Differential Dynamic Programming Algorithm with Path and Terminal Constraints
E Pellegrini, RP Russell
AAS/AIAA Astrodynamics Specialist Conference, Stevenson, WA, 2017
72017
Parallelized Sigma Point and Particle Filters for Navigation Problems
H Shen, V Vittaldev, CD Karlgaard, RP Russell, E Pellegrini
36th Annual AAS Guidance and Control Conference, 2013-034, 2013
72013
Multiple-shooting differential dynamic programming with applications to spacecraft trajectory optimization
E Pellegrini
42017
A multiple-shooting differential dynamic programming algorithm. Part 1: Theory
E Pellegrini, RP Russell
Acta Astronautica 170, 686-700, 2020
32020
Cycler Orbits and the Solar System Pony Express
MS Net, E Pellegrini, J Vander Hook
2020 IEEE Aerospace Conference, 1-10, 2020
12020
On the Accuracy of Trajectory State-Transition Matrices
E Pellegrini, RP Russell
AAS/AIAA Astrodynamic Specialist Conference, 2015
12015
F and G Taylor series solutions to the Circular Restricted Three Body Problem
E Pellegrini, RP Russell
24th AAS/AIAA Space Flight Mechanics Meeting, 2014, 559-573, 2014
1*2014
Parallel sigma point and particle filters for orbit determination
H Shen, C Karlgaard, RP Russell, V Vittaldev, E Pellegrini
Proceedings of the 9th US/Russian Space Surveillance Workshop, Krestovaya …, 2012
12012
Solar System Data Mules: Analysis for Mars and Jupiter
MS Net, E Pellegrini, W Parker, J Vander Hook
2021 IEEE Aerospace Conference (50100), 1-8, 2021
2021
A multiple-shooting differential dynamic programming algorithm. Part 2: Applications
E Pellegrini, RP Russell
Acta Astronautica 173, 460-472, 2020
2020
Data Mules on Cycler Orbits for High-Latency, Planetary-Scale Data Transfers
MS Net, E Pellegrini, J Vander Hook
2020
F and G Taylor series solutions to the Stark problem with Sundman transformations
E Pellegrini, RP Russell, V Vittaldev
2013 AAS/AIAA Astrodynamics Specialist Conference, Astrodynamics 2013, 369-388, 2014
2014
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