| Autor: |
Yaseri, Mohammadreza, Novinzadeh, Alireza Basohbat |
| Předmět: |
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| Zdroj: |
Proceedings of the Institution of Mechanical Engineers, Part G: Journal of Aerospace Engineering; Jun2024, Vol. 238 Issue 7, p647-667, 21p |
| Abstrakt: |
A model-free adaptive control is proposed for suboptimal guidance correction and control of a prototypical three-stage satellite carrier. For this sake, we consider a nominal guidance for the model of the system and design the adaptive control for a single-input multi-output system exposed to wind disturbance and measurement noise in the rates of inputs and outputs. Then, subsequent to the guidance correction, a differentiation model of the system is estimated and the control policy is realized under some profitable performance constraints to set the satellite in a desirable circular orbit. The simulation results readily reveal the efficiency of the proposed method and its robustness to uncertainties in the system. [ABSTRACT FROM AUTHOR] |
| Databáze: |
Complementary Index |
| Externí odkaz: |
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