Control of Distributed Space Systems
Lecture
Main Campus
Course Description
Keplerian orbital mechanics and orbital perturbations; the general relative motion problem; linear formation flying dynamics and control; impulsive station-keeping and reconfiguration; high order relative motion equations; formulation of relative motion using orbital elements; perturbation-invariant formations; nonlinear formation control; low-thrust propulsion for formation flying; relative navigation using GNSS and optical navigation; applications: sparse-aperture imaging, remote sensing, on-orbit servicing, rendezvous, and docking. Prerequisite: AA 242A, ENGR 105, AA 279A, and familiarity with MatLab.
AA 279D
Units: 3
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Typically Offered
Not Available
Grading Basis
Letter (ABCD/NP)
Class Level
Graduate
Instructional Mode
In Person
Gen Ed Requirement(s)
None
