Extremal Field Maps for Maneuverable Satellites: Reachability Analysis for Space Situational Awareness
Abstract
This grant is a continuation of research funded under a previous grant. This work will test the limits of the Picard iteration as a means of solving the equations of motion for satellites and optimize the code. In addition, a solution will be found to calculate the optimal parameters for a satellite to change orbit using the methods developed in the last grant.
Document Details
- Document Type
- DoD Grant Award
- Publication Date
- Mar 23, 2016
- Source ID
- FA95501510175
Entities
People
- John Junkins
Organizations
- Air Force Office of Scientific Research
- Texas Engineering Experiment Station
- United States Air Force