Flux-Pinned Dynamics Model Parameterization and Sensitivity Study
Author:
Affiliation:
1. Cornell University, Ithaca, New York 14853
2. Jet Propulsion Laboratory, California Institute of Technology, Pasadena, California 91109
Funder
NASA JPL Strategic Research
NASA Space Technology Research Fellowship
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Electrical and Electronic Engineering,Computer Science Applications,Aerospace Engineering
Reference39 articles.
1. Stability and Control of a Flux-Pinned Docking Interface for Spacecraft
2. Flux-Pinned Interfaces for the Assembly, Manipulation, and Reconfiguration of Modular Space Systems
3. Simulation of Multibody Spacecraft Reconfiguration through Sequential Dynamic Equilibria
4. Architecting the Very-Large-Aperture Flux-Pinned Space Telescope: A Scalable, Modular Optical Array with High Agility and Passively Stable Orbital Dynamics
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