This paper describes a general form of nonlinear dynamic inversion control for use in a generic nonlinear simulation to evaluate condidate augmented aircraft dynamics. The implementation is specifically tailored to the task of quickly assessing an aircraft's control power requirements and defining the achievable dynamic set.
Force and Moment Approach for Achievable Dynamics using Nonlinear Dynamics Inversion
1999
16 pages
Report
No indication
English
Force and Moment Approach for Achievable Dynamics Using Nonlinear Dynamic Inversion
British Library Conference Proceedings | 1999
|Aircraft Control Requirements and Achievable Dynamics Prediction
British Library Conference Proceedings | 1993
|Numerical Force Inversion in Floating Plate Dynamics
British Library Conference Proceedings | 2005
|