Development and analysis of a high fidelity linearized J₂ model for satellite formation flying
Thesis (S.M.)--Massachusetts Institute of Technology, Dept. of Aeronautics and Astronautics, 2001.
Main Author: | Schweighart, Samuel A. (Samuel Adam), 1977- |
---|---|
Other Authors: | Raymond J. Sedwick. |
Format: | Thesis |
Language: | eng |
Published: |
Massachusetts Institute of Technology
2013
|
Subjects: | |
Online Access: | http://hdl.handle.net/1721.1/82204 |
Similar Items
-
Electromagnetic formation flight dipole solution planning
by: Schweighart, Samuel A. (Samuel Adam), 1977-
Published: (2006) -
Micropropulsion system selection for precision formation flying satellites
by: Reichbach, Jeffrey (Jeffrey Grant), 1977-
Published: (2013) -
A real-time simulator for the SPHERES formation flying satellites testbed
by: Radcliffe, Andrew D. B. (Andrew Donald Brian), 1977-
Published: (2013) -
High-fidelity reduced-order aerodynamic models : application to active control of engine inlets
by: Lassaux, Guillaume, 1977-
Published: (2013) -
Model predictive control for formation flying spacecraft
by: Breger, Louis Scott, 1979-
Published: (2005)