کد مقاله | کد نشریه | سال انتشار | مقاله انگلیسی | نسخه تمام متن |
---|---|---|---|---|
4974702 | 1365545 | 2015 | 40 صفحه PDF | دانلود رایگان |
عنوان انگلیسی مقاله ISI
Sliding mode-based intercept guidance with uncertainty and disturbance compensation
ترجمه فارسی عنوان
هدایت رهگیری مبتنی بر حالت کشویی با عدم قطعیت و جبران خسارت
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موضوعات مرتبط
مهندسی و علوم پایه
مهندسی کامپیوتر
پردازش سیگنال
چکیده انگلیسی
This paper presents a missile intercept guidance law that can account for uncertainty and disturbance. The proposed guidance law is developed based on a novel second order sliding surface, along with an uncertainty and disturbance estimator. The proposed sliding surface is invariant for the non-impact angle constraint case as well as the impact angle constraint case. The sliding surface guarantees finite time convergence of the line-of-sight (LOS) rate and (if specified) the LOS angle error, characterized by a simple function of time-to-go. Furthermore, the proposed strategy is also effective against a maneuvering target. The line-of-sight rate convergence property can be adjusted using only one parameter that makes the design process simple. Potential of the proposed guidance laws is demonstrated with some simulations.
ناشر
Database: Elsevier - ScienceDirect (ساینس دایرکت)
Journal: Journal of the Franklin Institute - Volume 352, Issue 11, November 2015, Pages 5145-5172
Journal: Journal of the Franklin Institute - Volume 352, Issue 11, November 2015, Pages 5145-5172
نویسندگان
Takeshi Yamasaki, S.N. Balakrishnan, Hiroyuki Takano, Isao Yamaguchi,