کد مقاله کد نشریه سال انتشار مقاله انگلیسی نسخه تمام متن
4975864 1365594 2012 15 صفحه PDF دانلود رایگان
عنوان انگلیسی مقاله ISI
Robust H∞ control of spacecraft rendezvous on elliptical orbit
موضوعات مرتبط
مهندسی و علوم پایه مهندسی کامپیوتر پردازش سیگنال
پیش نمایش صفحه اول مقاله
Robust H∞ control of spacecraft rendezvous on elliptical orbit
چکیده انگلیسی
This paper investigates the robust H∞ control problem of spacecraft rendezvous on elliptical orbit. Based on Lyapunov theory, a sufficient condition for the existence of the robust H∞ controller is given in terms of the periodic Riccati differential equation (RDE). Then, a stabilizable controller design method based on a fast multi-shot algorithm is proposed. With the controller obtained, the spacecraft rendezvous mission can be accomplished. An illustrative example is provided to show the effectiveness of the proposed control design method.
ناشر
Database: Elsevier - ScienceDirect (ساینس دایرکت)
Journal: Journal of the Franklin Institute - Volume 349, Issue 8, October 2012, Pages 2515-2529
نویسندگان
, , ,