Adaptive Quaternion Attitude Control of Aerodynamic Flight Control Vehicles

S. M. Hoseini

Volume 11, Issue 2 , October 2017, , Pages 23-32

Abstract
  Conventional quaternion based methods have been extensively employed for spacecraft attitude control where the aerodynamic forces can be neglected. In the presence of aerodynamic forces, the flight attitude control is more complicated due to aerodynamic moments and inertia uncertainties. In this paper, ...  Read More