The Hypersonic International Flight Research Program (HIFiRE) is an international collaboration between the U.S. Air Force Research Laboratory and the Defence Science Technology Organisation in Australia. The HIFiRE program is investigating basic hypersonic phenomena and experimental technologies critical to the development of next generation aerospace vehicles and the understanding of the environments in which they must operate. Further this program will advance the state-of-the-art in a number of disciplines by progressively evaluating component technologies having increasing levels of complexity and likeness to those of expected operational systems. The approach is to utilize sounding rockets in order to mature a low-cost approach to hypersonic flight test. To this end, HIFiRE 6 will evaluate the tracking performance of an adaptive flight control system on a representative hypersonic vehicle that is executing a set of predefined maneuvers. This paper describes the current HIFiRE 6 mission and vehicle system to execute the experiment, along with a description of the adaptive control law and simulation results.
[1]
L. Praly,et al.
Adaptive nonlinear regulation: estimation from the Lyapunov equation
,
1992
.
[2]
E. Lavretsky,et al.
Adaptive control of flight: theory, applications, and open problems
,
2006,
2006 American Control Conference.
[3]
Allan Paull,et al.
HIFiRE 4: A low-Cost Aerodynamics, Stability, and Control Hypersonic Flight Experiment
,
2011
.
[4]
Kevin Wise,et al.
Robust Stability Analysis of Adaptive Missile Autopilots
,
2008
.
[5]
John Hodgkinson,et al.
Hypersonic Stability Derivative Modeling Issues
,
2010
.
[6]
Eugene Lavretsky,et al.
Adaptive Control and the NASA X-15-3 Flight Revisited
,
2010,
IEEE Control Systems.
[7]
D. Levandier,et al.
Approved for Public Release; Distribution Unlimited
,
1994
.
[8]
Michael Richard,et al.
The X-43A Six Degree of Freedom Monte Carlo Analysis
,
2008
.