Direct neural discrete control of hypersonic flight vehicle

• المؤلفون الرئيسيون: Xu, Bin, Wang, Danwei, Sun, Fuchun, Shi, Zhongke
• مؤلفون آخرون: School of Electrical and Electronic Engineering
• التنسيق: مقال
• اللغة: English
• منشور في: 2013
• الموضوعات: DRNTU::Engineering::Electrical and electronic engineering
• الوصول للمادة أونلاين: https://hdl.handle.net/10356/98203; http://hdl.handle.net/10220/17651

This paper investigates the discrete neural control for flight path angle and velocity of a generic hypersonic flight vehicle (HFV). First, strict-feedback form is set up for the attitude subsystem considering flight path angle, pitch angle, and pitch rate by altitude-flight path angle transformatio...