Asymmetric Barrier Lyapunov Function based Practical Fixed-time Control of Vertical Take-off/ Vertical Landing Reusable Launch Vehicles with Partial State Constraints

被引：3

作者：

Ju, Xiaozhe ^{[1
]}

Wang, Feng ^{[1
]}

Wei, Changzhu ^{[1
]}

Zhang, Liang ^{[2
]}

机构：

[1] Harbin Inst Technol, Sch Astronaut, Harbin 150001, Peoples R China

[2] Sun Yat Sen Univ, Sch Aeronaut & Astronaut, Guangzhou 510275, Peoples R China

来源：

IFAC PAPERSONLINE | 2020年 / 53卷 / 02期

关键词：

Vertical take-off/ vertical landing; aerodynamic guidance phase; partial state constraints; practical fixed-time; asymmetric logarithm-type barrier function; asymmetric double-exponential-type barrier function; ADAPTIVE-CONTROL;

D O I：

10.1016/j.ifacol.2020.12.1929

中图分类号：

TP [自动化技术、计算机技术];

学科分类号：

0812 ;

摘要：

In order to stabilize the vertical take-off/ vertical landing reusable launch vehicles in aerodynamic guidance phase against complex disturbances and partial state constraints, an asymmetric logarithm-type barrier function and asymmetric double-exponential-type barrier function are proposed, where the latter is smooth with respect to system states and has a higher application value compared with the logarithm-type one. Based on the barrier functions and practical fixed-time control theory, two practical fixed-time control laws are derived to drive the attitude tracking errors to a small neighborhood of the origin within a fixed time and ensure the attitude constraints unviolated. Simulation results demonstrate the efficiency of the controllers. Copyright (C) 2020 The Authors.

引用

页码：14845 / 14850

页数：6

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