Date of Award
Fall 12-2015
Access Type
Thesis - Open Access
Degree Name
Master of Science in Aerospace Engineering
Department
Aerospace Engineering
Committee Chair
M.J. Balas
First Committee Member
Darris White
Second Committee Member
Bogdan Udrea
Third Committee Member
Richard Prazenica
Abstract
In this paper we explore a Direct Adaptive Control scheme for stabilizing a non-linear, physics based model of the longitudinal dynamics for an air breathing hypersonic vehicle. The model, derived from first principles, captures the complex interactions between the propulsion system, aerodynamics, and structural dynamics. The linearized aircraft dynamics show unstable and non-minimum phase behavior. It also shows a strong short period coupling with the fuselage-bending mode. The value added by direct adaptive control and the theoretical requirements for stable convergent operation is displayed. One of the main benefits of the Directive Adaptive Control is that it can be implemented knowing very little detail about the plant. The implementation uses only measured output feedback to accomplish the adaptation. A stability analysis is conducted on the linearized plant to understand the complex aero-propulsion and structural interactions. The multivariable system possesses certain characteristics beneficial to the adaptive control scheme; we discuss these advantages and ideas for future work.
Scholarly Commons Citation
Aditya, Ron, "Direct Adaptive Control for Stability and Command Augmentation System of an Air-Breathing Hypersonic Vehicle" (2015). Doctoral Dissertations and Master's Theses. 191.
https://commons.erau.edu/edt/191
