Neural Extended State Observer Based Intelligent Integrated Guidance and Control for Hypersonic Flight

Near-pace hypersonic flight has great potential in civil and military use due to its high speed and low cost. To optimize the design and improve the robustness, this paper focuses on the integrated guidance and control (IGC) design with nonlinear actuator dynamics in the terminal phase of hypersonic...

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Bibliographic Details
Main Authors: Liang Wang, Ke Peng, Weihua Zhang, Donghui Wang
Format: Article
Language:English
Published: MDPI AG 2018-09-01
Series:Energies
Subjects:
Online Access:http://www.mdpi.com/1996-1073/11/10/2605