Dr. Pyare Mohan Tiwari(Link)
Electrical and Electronics Engineering, Amity University Uttar Pradesh
Title: Spacecraft Attitude Control using Efficient Sliding Mode Control
Abstract:Success of spacecraft mission is significantly dependent on efficient attitude control design. Spacecraft attitude control problem is addressed enough taking different control strategies. However, robustness, pointing accuracy, and quick orientation are the still major issues to be addressed with more care. Sliding mode control is an inherently robust control methods with simple design method. Recent advancement in sliding mode techniques motivate to explore its uses for spacecraft attitude control design. This talk aims to discuss the issues on sliding mode-based attitude control design with novel control structures to make attitude control system more efficient.
Brief introduction
PhD from Indian Institute of Technology, Delhi
Total teaching and research experience 16 years
Presently working in area of Sliding Mode Control Engineering and its Applications. Significant contribution is done to apply sliding mode control engineering for Spacecraft Attitude Control Design