Distributed Attitude Control for Multispacecraft via Takagi-Sugeno Fuzzy Approach

This paper investigates the problem of distributed attitude control for spacecraft formation flying systems based on the Takagi-Sugeno (T-S) fuzzy modeling method, where external disturbances and parameter uncertainties are considered. The spacecraft attitude dynamics is constructed as T-S fuzzy model and a modified distributed fuzzy-based H-infinity controller is designed. It is proven that the attitude of multispacecraft can synchronously reach zero by using the designed controller. Numerical examples are provided to illustrate the effectiveness of the proposed controller and comparisons with the existing results.