Journal of Space Science and Technology

Journal of Space Science and Technology

Kinematic Modelling Without Singularity and Nonlinear Control of Satellite Attitude Using Direct Adaptive and Fuzzy PD Control Methods

Document Type : Original Research Paper

Authors
Mohammad Navabi 1
Nazanin Safaei Hashekvaei 2
1 Associate Professor, Faculty of New Technologies Engineering, Shahid Beheshti University, Tehran, Iran
2 Faculty of New Technologies Engineering, Shahid Beheshti University, Tehran, Iran
10.22034/jsst.2021.1248
Abstract
Adaptive control technique is taken into consideration because of overcoming the problem of existence of uncertainties in the space missions. In this paper, a novel optimal direct adaptive control technique which is based on Markov parameters is presented. In this technique, the system's performance is expressed based on rotation matrices, and this method doesn't have a singularity problem. The problem of satellite attitude control using this method and nonlinear thruster actuator in existence of uncertainty in moment of inertia is analyzed. The novel adaptive controller using on-off thrusters is robust to inertia changes. In this paper, a mamdani fuzzy logic is used to schedule the gains of PD control method, and the satellite attitude control problem using a fuzzy controller is simulated. With considering the settling and rise times, it's shown that the fuzzy controller is better than the presented adaptive controller. Also, the problem of satellite attitude control using the novel adaptive controller in presence of a constant disturbance is analyzed, and simulation results illustrate that the new adaptive control is robust to a constant disturbance.
Keywords
Satellite attitude
optimal adaptive control
on-off thrusters
fuzzy controller
constant disturbance
Subjects

Article Title Persian

مدل‌سازی سینماتیکی بدون تکینگی و کنترل غیرخطی وضعیت ماهواره با استفاده از روش کنترل تطبیقی مستقیم و PD فازی

Authors Persian

محمد نوابی 1
نازنین صفایی حشکوائی 2
1 دانشیار، دانشکده مهندسی فناوری های نوین، دانشگاه شهید بهشتی، تهران، ایران
2 دانشکده مهندسی فناوری های نوین، دانشگاه شهید بهشتی، تهران، ایران
Abstract Persian

روش کنترل تطبیقی به دلیل غلبه بر مشکل وجود عدم قطعیت‌ها در مأموریت‌های فضایی مورد توجه قرار می‌گیرد. در این مقاله یک روش کنترل تطبیقی مستقیم بهینه نوین که بر اساس پارامترهای مارکوف طراحی می‌گردد جهت کنترل وضعیت ماهواره ارائه می‌شود، و مسئله کنترل وضعیت ماهواره با استفاده از این روش کنترلی و عملگر تراستر غیرخطی در حضور نامعینی‌های ممان اینرسی بررسی می‌گردد. در روش کنترلی ارائه شده عملکرد سیستم بر اساس ماتریس‌های دوران بیان می‌شود، و این روش مشکل سینگولاریتی ندارد. جهت مقایسه روش معرفی شده با سایر روش‌های کنترلی، کنترل وضعیت ماهواره با استفاده از کنترلر فازی شبیه‌سازی می‌گردد، و در نهایت برتری روش کنترلی فازی نسبت به روش کنترل تطبیقی بیان شده با در نظر گرفتن زمان صعود و نشست سیستم نشان داده می‌شود. همچنین نتایج حاصل از شبیه‌سازی‌ها نشان می-دهند که روش کنترل تطبیقی ارائه شده با استفاده از عملگر تراستر روشن-خاموش نسبت به عدم قطعیت در اینرسی مقاوم است.

Keywords Persian

مدل‌سازی سینماتیکی بدون تکینگی
کنترل وضعیت
عملگر تراستر روشن-خاموش
کنترل تطبیقی مستقیم
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  • Receive Date 07 December 2019
  • Revise Date 20 May 2020
  • Accept Date 14 October 2020
  • First Publish Date 14 November 2020