摘要: High bandwidth sensing devices such as LiDAR have capabilities to measure the velocity components of turbulent gust before an aircraft is penetrated into it. Gust is therefore proportional to the state variables of the aircraft. I... 展开 High bandwidth sensing devices such as LiDAR have capabilities to measure the velocity components of turbulent gust before an aircraft is penetrated into it. Gust is therefore proportional to the state variables of the aircraft. It eventually gets augmented to the system dynamic matrix as the real parameter variations, which are the stochastic stability derivatives available to characterize the forces and moments acting on the aircraft. The combat and transport aircraft transient responses to gust with these measurable forces and moments, by the approach, are not controllable by the inner loop because it is meant to generate the steady-state trim deflections. Moreover, transient response control is a high bandwidth control problem. Given these concerns, in this paper, some foundations for ride quality regulation based on the bandwidth modulated structured compensators are presented for accommodation into the inner loop control structure. We provide a new procedure to design structured compensators, in case, high frequency actuation demanded at the miniature flow control effectors distributed across the wing is required. Features such as the gust itself becoming a transient command input generator for alleviation are discussed. The analysis is shown to be an important input to control the wing loading and enhance smooth aircraft ride quality in the turbulent time windows. 收起