Robust Adaptive Flight Control Design of Air-breathing Hypersonic Vehicles
Abstract
The main objective of this research is to propose innovative nonlinear adaptive controllers for hypersonic vehicles, which can be ‘substantially robust’ to the modeling inaccuracy of the vehicle dynamics, thereby minimizing the necessity to have a very high fidelity model.
Document Details
- Document Type
- DoD Grant Award
- Publication Date
- Mar 23, 2016
- Source ID
- FA23861514045
Entities
People
- Radhakant Padhi
Organizations
- Air Force Office of Scientific Research
- Indian Institute of Science, Bengaluru
- United States Air Force