کد مقاله کد نشریه سال انتشار مقاله انگلیسی نسخه تمام متن
710309 892108 2016 6 صفحه PDF دانلود رایگان
عنوان انگلیسی مقاله ISI
Altitude Control for Small Fixed-Wing Aircraft Using H∞ Loop-Shaping Method
موضوعات مرتبط
مهندسی و علوم پایه سایر رشته های مهندسی مکانیک محاسباتی
پیش نمایش صفحه اول مقاله
Altitude Control for Small Fixed-Wing Aircraft Using H∞ Loop-Shaping Method
چکیده انگلیسی

Autopilot systems for UAVs without human pilots maintain the flight through an appropriate balance of aerodynamic forces autonomously. That is to say, they are used to make flight missions more reliable and efficient. Autopilot system design architecture conventionally contains two sections, inner and outer loops. Inner loop is the stabilizer and the outer loop can provide one of the additional motion controls (or all) such as speed, altitude, and heading hold. In this paper, H∞ Loop-shaping method is used to provide the stabilizer mode and the PID controller is used to control the altitude.

ناشر
Database: Elsevier - ScienceDirect (ساینس دایرکت)
Journal: IFAC-PapersOnLine - Volume 49, Issue 9, 2016, Pages 111–116
نویسندگان
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