DYNAMIC TERMINAL SLIDING MODE CONTROL FOR AN AEROSPACE LAUNCH VEHICLE

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ALIKHANI A.; KASAEIAN S.A.

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Paper Information

Journal: Journal of Space Science and Technology Year:2016 | Volume:8 | Issue:4 Page(s): 1-7

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Title

DYNAMIC TERMINAL SLIDING MODE CONTROL FOR AN AEROSPACE LAUNCH VEHICLE

Author(s)

ALIKHANI A. | KASAEIAN S.A. | Issue Writer Certificate

Keywords

TERMINAL SLIDING MODEQ2

DYNAMIC SLIDING MODEQ2

UNMATCHED DISTURBANCEQ2

FINITE-TIME CONVERGENCEQ2

Abstract

Tracking guidance commands for a time-varying aerospace launch vehicle during the atmospheric flight is considered in this paper. Hence, the dynamic TERMINAL SLIDING MODE control law is constructed for this purpose and DYNAMIC SLIDING MODE control is utilized.The terminal sliding manifold causes the DYNAMIC SLIDING MODE to converge asymptotically to zero in finite-time. The actuator and rate gyro dynamics are included in the model of launch vehicle. DYNAMIC SLIDING MODE control accommodates UNMATCHED DISTURBANCEs, while the TERMINAL SLIDING MODE control is used to accelerate the system to reach the dynamic sliding manifold. Finally, the effectiveness of the proposed control is demonstrated in the presence of UNMATCHED DISTURBANCEs and is compared with the DYNAMIC SLIDING MODE.

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APA: Copy

ALIKHANI, A., & KASAEIAN, S.A.. (2016). DYNAMIC TERMINAL SLIDING MODE CONTROL FOR AN AEROSPACE LAUNCH VEHICLE. JOURNAL OF SPACE SCIENCE AND TECHNOLOGY (JSST), 8(4), 1-7. SID. https://sid.ir/paper/149878/en

Vancouver: Copy

ALIKHANI A., KASAEIAN S.A.. DYNAMIC TERMINAL SLIDING MODE CONTROL FOR AN AEROSPACE LAUNCH VEHICLE. JOURNAL OF SPACE SCIENCE AND TECHNOLOGY (JSST)[Internet]. 2016;8(4):1-7. Available from: https://sid.ir/paper/149878/en

IEEE: Copy

A. ALIKHANI, and S.A. KASAEIAN, “DYNAMIC TERMINAL SLIDING MODE CONTROL FOR AN AEROSPACE LAUNCH VEHICLE,” JOURNAL OF SPACE SCIENCE AND TECHNOLOGY (JSST), vol. 8, no. 4, pp. 1–7, 2016, [Online]. Available: https://sid.ir/paper/149878/en

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