در این مقاله به ارائه یک رویکرد جدید در طراحی کنترلکننده وضعیت یک ماهواره با استفاده از چرخهای عکسالعملی پرداخته شده است. ابتدا یک کنترلکننده غیرخطی که بهرههای آن در هر لحظه وابسته به متغیرهای حالت است پیشنهاد میگردد. در گام اول، روند استخراج ضرایب کنترل با استفاده از بهینهساز GA تشریح میگردد. سپس با استفاده از نتایج تعدادی آزمایش، داده کافی برای شبه مدلسازی (Meta Modelling) سیستم استخراج شده و با استفاده از بانک دادهها، تابع بهرههای کنترلی مربوطه بهینهسازی میگردند. ورودی تابع مذکور حالتهای سیستم و خروجی آن ضرایب کنترلی است. در نهایت از یک پلتفرم شبیهساز تعیین و کنترل وضعیت ماهواره مبتنی بر یاتاقان هوایی جهت ارزیابی رویکرد پیشنهادی استفاده گردید. نتایج تست آزمایشگاهی نشان میدهد عملکرد روش پیشنهاد شده تا 30% بهتر از کنترل کننده کلاسیک PID با ضرایب ثابت است.
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