A multi-year research effort to develop and validate a feedback algorithm for medium range air-to-air interceptions with realistic capture conditions, compatible with the deployment of advanced guided weapons in a future air combat scenario is summarized. Previous work is reviewed and new results are presented. The proposed guidance algorithm is based on the application of singular perturbation techniques. The examples included, featuring both previous generation (F-4) and state of the art (F-15) fighter aircraft models, demonstrate the structural robustness of the feedback guidance laws. The hierarchical structure of the algorithm, the explicit feedback form of the control laws and the validated high accuracy, make the algorithm a very attractive candidate for a real time implementation on board a future interceptor aircraft.
Synthesis and Validation of Feedback Guidance Laws for Air-to-Air Interceptions
1990
69 pages
Report
No indication
English
TECHNOLOGIE - Premières interceptions du Spyder
Online Contents | 2005
MISSILES - Interceptions de missiles balistiques sur le Pacifique.
Online Contents | 1999
Optimal Interceptions on Two-Dimensional Grids with Obstacles
Online Contents | 2008
|