Simba, Ashutosh and Padhi, Radhakant (2016) A New Philosophy in Adaptive Control Design for Robust Attitude Maneuver of Spacecrafts. In: 4th IFAC Conference on Advances in Control and Optimization of Dynamical Systems (ACODS 2016), FEB 01-05, 2016, Tiruchirappalli, INDIA, pp. 682-687.
IFAC_Pap_49-1_682_2016.pdf - Published Version
Restricted to Registered users only
Download (1052Kb) | Request a copy
An adaptive control law has been designed for robust attitude tracking of a spacecraft with uncertain inertia matrix, torque coupling; coefficients and exogenous disturbances. The strict block feedback structure of the attitude dynamics is exploited in designing a back stepping control law, which depends on a compensator variable whose dynamics is designed to adapt to the unknown parameters. Two switching components have been incorporated into the dynamic feedback law to ensure robustness with respect to the disturbances and uncertainties in the torque coupling; coefficients. The spacecraft dynamics is simulated using the dynamic feedback control, first without the switching components and later incorporating the same, in order to demonstrate the effectiveness and robustness of the proposed method. (C) 2016, IFAC (International Federation of Automatic Control) Hosting by Elsevier Ltd. All rights reserved.
|Item Type:||Conference Proceedings|
|Additional Information:||Copy right for this article belongs to the ELSEVIER SCIENCE BV, PO BOX 211, 1000 AE AMSTERDAM, NETHERLANDS|
|Keywords:||Adaptive control; Robust Control; Attitude Tracking; Dynamic Feedback|
|Department/Centre:||Division of Mechanical Sciences > Aerospace Engineering (Formerly, Aeronautical Engineering)|
|Date Deposited:||20 Jul 2016 09:00|
|Last Modified:||20 Jul 2016 09:00|
Actions (login required)