A Novel Computational Framework for Optimal Control of Partial Differential Equations Using Gaussian Quadrature Orthogonal Collocation Methods
Abstract
The objective of this effort is to address the development of computational trajectory optimization methods relevant to high-speed flight systems coupled tightly with the response of a thermal protection system (TPS) containing multiple materials with temperature dependent properties governed by the transient heat equation.
Document Details
- Document Type
- DoD Grant Award
- Publication Date
- Feb 07, 2025
- Source ID
- FA86512510002
Entities
People
- Anil V. Rao
Organizations
- Air Force Research Laboratory
- United States Air Force
- University of Florida