کنترل مد لغزشی ترمینال تطبیقی بدون تکینگی و مبتنی بر رؤیتگر اغتشاش برای کنترل سیستم ژیروسکوپ ارتعاشی میکروالکترومکانیک
محورهای موضوعی : مهندسی برق و کامپیوتر
1 - دانشگاه علوم و فنون هوایی شهید ستاری
چکیده مقاله :
در این مقاله، یک کنترل‌کننده مد لغزشی ترمینال تطبیقی بدون تکینگی مبتنی بر رؤیتگر اغتشاش برای فرایند تشخیص و کنترل فرایند تحریک سیستم ژیروسکوپ ارتعاشی میکروالکترومکانیک پیشنهاد می‌شود. بدین منظور در ابتدا معادلات دینامیکی سیستم ژیروسکوپ ارتعاشی بیان می‌گردد. در ادامه معادلات دینامیکی این سیستم به حوزه معادلات حالت و سپس به حوزه خطای ردگیری انتقال داده می‌شود. پس از آن ساختار دینامیکی رؤیتگر اغتشاش زمان محدود ارائه می‌گردد. سپس روش طراحی کنترل مد لغزشی ترمینال تطبیقی بدون تکینگی و مبتنی بر رؤیتگر اغتشاش زمان محدود بیان می‌شود. راهکار پیشنهادی کنترل فرایند تحریک را در حضور عدم قطعیت‌های ساختاری و غیر ساختاری موجود در معادلات دینامیکی سیستم ژیروسکوپ ارتعاشی میکروالکترومکانیکی انجام می‌دهد و فرایند تشخیص از طریق تنها یک قانون تطبیقی انجام می‌گردد. اثبات ریاضی نشان می‌دهد که سیستم حلقه بسته با کنترل پیشنهادی و در حضور عدم قطعیت‌های موجود، دارای پایداری مجانبی سراسری زمان محدود است. حضور رؤیتگر اغتشاش در ساختار کنترل پیشنهادی باعث می‌شود تا نقش عدم قطعیت‌های غیر ساختاری در فرایند کنترل سیستم ژیروسکوپ را تضعیف نماید و دامنه ورودی کنترل را نیز کاهش دهد. برای بررسی عملکرد کنترل پیشنهادی، شبیه‌سازی‌هایی در 3 مرحله بر روی سیستم ژیروسکوپ ارتعاشی الکترومکانیک پیاده‌سازی می‌گردد. نتایج شبیه‌سازی‌ها، عملکرد مطلوب راهکار پیشنهادی را تأیید می‌نمایند.
In this paper, an adaptive non-singular terminal sliding mode control based on disturbance observer is proposed for detection process and control of the micro-electromechanical vibratory gyroscope stimulation process. For this purpose, the dynamical equations of the vibrational gyroscope system are initially expressed. In the following, the dynamical equations of this system are transmitted to the domain of state-space equations and then to the domain of tracking error. After that, the dynamic structure of the finite time disturbance observer is presented. Then, the design of the adaptive non-singular terminal sliding mode control based on finite time disturbance observer is expressed. The proposed strategy carries out the control of the stimulation process in the presence of structured and un-structured uncertainties existing in the dynamic equations of the microelectromechanical vibrational gyroscope system, and performs the detection process through only an adaptive law. The mathematical proof shows that the closed-loop system with the proposed control, and in the presence of the existing uncertainties, has the finite time global asymptotic stability. The presence of a disturbance observer in the proposed control structure will weaken the role of un-structured uncertainties in the gyroscope control process and reduce the control input amplitude. In order to evaluate the proposed control performance, simulations in 3 steps are implemented on the electromechanical vibrational gyroscope system. Simulation results confirm the desired performance of the proposed control.
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