Abstract
Abstract: The colony of a celestial universe has become foremost task for many countries in the late decades. The spinning attitude control for economical satellite operation is widely used. This paper shows a successful implementation of state space technique to inherently unstable satellite spun around longitudinal axis. Full-state feedback and reference input with full-state feedback are compared for deadbeat response. The state space control gains are tuned to satisfy controllability conditions. Observability conditions are checked for better tracking of attitude spinning angle to step input with the aim to achieve a robust spin stabilization of the satellite manoeuvre. Satisfactory deadbeat specifications are obtained based on reference input with full-state feedback. However, full-state feedback implements reasonable design gains and it appears to be slower in judgment with reference input with full-state feedback gains. The simulation and analytical results are well agreed based on dominant second-order poles.
Keywords
Spinning Satellite Stabilization Deadbeat Control State Space Pole Placement Method FSF and RIFSF controllers
References
- Gene F. Frankin, J. David Powell, and Abbas Emami-Naeini (2010). Feedback Control of Dynamic Systems. 6th ed. Pearson Prentice HallTM.
- Buckley, G.J. (1990). Modern Control Started with Ziegler-Nichols Tuning. Control Engineering, 2nd Edition, Vol. 37, No. 12, pp. 11-17.
- Wittenmark, B. (1979). Self -tuning PID Controllers Based on Pole Placement. Lund Inst. of Technology. Report No. TFRT-7179.
- Kuo, Benjamin C (1994). 1930- MATLAB tools for control system analysis and design. Englewood Cliffs, NJ. Prentice Hall, 0130346462
- Tsiotras, P. 1996). Stabilisation and Optimality Results for the Attitude Control Problem. Journal of Guidance, Control, and Dynamics, Vol. 19, No. 4.
- Dorf, C.R. (1989). Modern Control Systems. 5th edition Reading, Ma. Addison- Wesley
- E. Finlay-Freundlich (1958). Celestial Mechanics. Pergamon press.
- Fortescue, M. (1996). Spacecraft Systems Engineering. McGraw Hill.
- Peter Fortescue. (1994). Spacecraft Systems Engineering. Wiley Publishers.
Abstract
References
- Gene F. Frankin, J. David Powell, and Abbas Emami-Naeini (2010). Feedback Control of Dynamic Systems. 6th ed. Pearson Prentice HallTM.
- Buckley, G.J. (1990). Modern Control Started with Ziegler-Nichols Tuning. Control Engineering, 2nd Edition, Vol. 37, No. 12, pp. 11-17.
- Wittenmark, B. (1979). Self -tuning PID Controllers Based on Pole Placement. Lund Inst. of Technology. Report No. TFRT-7179.
- Kuo, Benjamin C (1994). 1930- MATLAB tools for control system analysis and design. Englewood Cliffs, NJ. Prentice Hall, 0130346462
- Tsiotras, P. 1996). Stabilisation and Optimality Results for the Attitude Control Problem. Journal of Guidance, Control, and Dynamics, Vol. 19, No. 4.
- Dorf, C.R. (1989). Modern Control Systems. 5th edition Reading, Ma. Addison- Wesley
- E. Finlay-Freundlich (1958). Celestial Mechanics. Pergamon press.
- Fortescue, M. (1996). Spacecraft Systems Engineering. McGraw Hill.
- Peter Fortescue. (1994). Spacecraft Systems Engineering. Wiley Publishers.
Details
| Primary Language | English |
|---|---|
| Journal Section | Research Article |
| Authors | |
| Publication Date | June 29, 2015 |
| Published in Issue | Year 2015 Volume: 3 Issue: 3 |
