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作者机构:Harbin Inst Technol Space Control & Inertial Technol Res Ctr Harbin 150001 Peoples R China Harbin Inst Technol Ctr Composite Mat & Struct Harbin 150001 Peoples R China
出 版 物:《AEROSPACE SCIENCE AND TECHNOLOGY》 (航宇科学与技术)
年 卷 期:2020年第104卷
页 面:105936-105936页
核心收录:
学科分类:08[工学] 0825[工学-航空宇航科学与技术]
主 题:Hypersonic vehicle Longitudinal control Hybrid actuators Simplified algorithm
摘 要:This paper considers the longitudinal compound control of air-breathing hypersonic vehicles configured with hybrid aerodynamic control surface (ACS) and reaction control system (RCS). In the altitude loop, the proposed nonadaptive back-stepping design results in a simplified ACS-RCS compound control. This is attributable to the introduced tangent tracking errors and ACS-RCS fusion algorithm. ACS nonlinearity, RCS quantization, and modeling parametric uncertainties are handled. In the velocity loop, the performance guaranteed adaptive control is enhanced with the bound estimation mechanism, which accommodates modeling parametric uncertainties with a low dynamic order. The effectiveness of the proposed control is verified via simulations. (C) 2020 Elsevier Masson SAS. All rights reserved.