Block Dynamic Surface Control Applied to a Sea-Skimming Missile

被引：5

作者：

Almeida Coelho, Fernando Antonio ^{[1
]}

Hemerly, Elder Moreira ^{[2
]}

机构：

[1] Marinha Brasil, Weapon Syst Directorate, 21 Andar Ctr,R Primeiro de Marco,118, BR-20010000 Rio De Janeiro, Brazil

[2] Inst Tecnol Aeronaut, Syst & Control Dept, Praca Mal Eduardo 50, BR-12228900 Sao Jose De Campos, Brazil

来源：

JOURNAL OF GUIDANCE CONTROL AND DYNAMICS | 2017年 / 40卷 / 05期

关键词：

AUTOPILOT DESIGN;

D O I：

10.2514/1.G002298

中图分类号：

V [航空、航天];

学科分类号：

08 ; 0825 ;

摘要：

Researchers propose to keep the nonlinear body-axes six-degree-of-freedom (6-DOF) model by grouping the states variables into two separate row vectors: one for kinematics and the other for dynamics equations. By doing this, the equations appear in a blockstrict-feedback form. The backstepping approach is employed to solve this problem. As the characteristics nonlinearity and the coupling of the attitude channels are not added to the uncertainty term, it has smaller amplitude, demanding less control action and producing a more robust control system.

引用

页码：1283 / U214

页数：7

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