ASCENDING PHASE FUZZY LOGIC GUIDANCE OF SATELLITE LAUNCH VEHICLES FOR REDUCING THE ADVERSE WIND EFFECTS

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SOHRAB M.; ZARDASHTI R.; JALALI NAINI S.H.

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Journal Paper

Paper Information

Journal: Journal of Space Science and Technology Year:2014 | Volume:7 | Issue:3 Page(s): 75-82

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Information Journal Paper

Title

ASCENDING PHASE FUZZY LOGIC GUIDANCE OF SATELLITE LAUNCH VEHICLES FOR REDUCING THE ADVERSE WIND EFFECTS

Author(s)

SOHRAB M. | ZARDASHTI R. | JALALI NAINI S.H. | Issue Writer Certificate

Keywords

LAUNCH VEHICLEQ2

FUZZY GUIDANCEQ2

ASCEND PHASEQ2

WIND EFFECTQ2

Abstract

In this paper, a fuzzy logic guidance algorithm is presented for the ascending phase of satellite LAUNCH VEHICLEs in the presence of WIND EFFECTs. In this algorithm, the midcourse constraints including maximum allowable angle of attack at the maximum dynamic pressure and the product of the dynamic pressure and angle of attack, as well as constraints on the final altitude and flight-path angle are considered. The algorithm uses a Mamdani- type fuzzy controller with centroid defuzzification. Maximizing and minimizing set methods to reduce WIND EFFECT, while satisfying the midcourse and final constraints. Simulation results show that the presented algorithm improves the performance of the satellite LAUNCH VEHICLE, satisfying the constraints within the maximum allowable estimation error on wind speed.

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APA: Copy

SOHRAB, M., ZARDASHTI, R., & JALALI NAINI, S.H.. (2014). ASCENDING PHASE FUZZY LOGIC GUIDANCE OF SATELLITE LAUNCH VEHICLES FOR REDUCING THE ADVERSE WIND EFFECTS. JOURNAL OF SPACE SCIENCE AND TECHNOLOGY (JSST), 7(3 ), 75-82. SID. https://sid.ir/paper/149990/en

Vancouver: Copy

SOHRAB M., ZARDASHTI R., JALALI NAINI S.H.. ASCENDING PHASE FUZZY LOGIC GUIDANCE OF SATELLITE LAUNCH VEHICLES FOR REDUCING THE ADVERSE WIND EFFECTS. JOURNAL OF SPACE SCIENCE AND TECHNOLOGY (JSST)[Internet]. 2014;7(3 ):75-82. Available from: https://sid.ir/paper/149990/en

IEEE: Copy

M. SOHRAB, R. ZARDASHTI, and S.H. JALALI NAINI, “ASCENDING PHASE FUZZY LOGIC GUIDANCE OF SATELLITE LAUNCH VEHICLES FOR REDUCING THE ADVERSE WIND EFFECTS,” JOURNAL OF SPACE SCIENCE AND TECHNOLOGY (JSST), vol. 7, no. 3 , pp. 75–82, 2014, [Online]. Available: https://sid.ir/paper/149990/en

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