Adaptive Missile Flight Control for Complex Aerodynamic Phenomena

Report No. ARL-TR-8085
Authors: Frank Fresconi; Ben Gruenwald; Tansel Yucelen; Jubaraj Sahu
Date/Pages: August 2017; 40 pages
Abstract: The goal of this research is to formulate flight controllers for highly maneuverable munitions. Complex aerodynamic phenomena such as vortex interactions and flow separation exist on munitions flying at certain maneuvering conditions. Aerodynamic models are proposed to capture these mechanisms within an adaptive control framework. The adaptive control algorithm is derived and wrapped around a nominal optimal controller using inertial sensor feedback. The vehicle dynamics and flight control algorithms are implemented in simulation. Results indicate that only the adaptive algorithm recovers satisfactory control when encountering these complex aerodynamic phenomena.
Distribution: Approved for public release
  Download Report ( 4.065 MBytes )
If you are visually impaired or need a physical copy of this report, please visit and contact DTIC.

Last Update / Reviewed: August 1, 2017