A Data-based Performance Evaluation Method for Aircraft Attitude Control System

被引：0

作者：

Wang, Yuxiao ^{[1
]}

Zhao, Yuyu ^{[1
]}

机构：

[1] Civil Aviat Univ China, Coll Elect Informat & Automat, Tianjin 300300, Peoples R China

来源：

2021 PROCEEDINGS OF THE 40TH CHINESE CONTROL CONFERENCE (CCC) | 2021年

关键词：

Aircraft Attitude Control System; Performance Evaluation; Indicator System; Indicator Calculation Methods; Multi-indicator Synthesize;

D O I：

暂无

中图分类号：

TP [自动化技术、计算机技术];

学科分类号：

0812 ;

摘要：

The attitude control systems play an extremely important role in flight control systems. In order to ensure the safety and stability of flight control system, it is necessary to evaluate the performance of attitude control system effectively. In this paper, a data-based performance evaluation method for aircraft attitude control system performance is proposed. The structure of the aircraft attitude control system is analyzed, a hierarchical performance evaluation indicator system is established, and the calculation method for each lowest indicator is given. Considering the equilibrium of the system in the evaluation, a variable weight determination method is proposed. A supporting evaluation tool is developed, through which an example of aircraft attitude control system performance evaluation is given and the result of the evaluation example is analyzed which is benefit to the study of the performance evaluation of aircraft attitude control systems.

引用

页码：6691 / 6696

页数：6

共 9 条

[1]

AHUJA LR, 2000, AIAA GUID NAV CONTR, P1

[2]

FU R, 2009, J HUAZHONG U SCI TEC, P19, DOI DOI 10.1109/IACSIT-SC.2009.85

[3] Test results for entry guidance methods for space vehicles [J].

Hanson, JM ;

Jones, RE .

JOURNAL OF GUIDANCE CONTROL AND DYNAMICS, 2004, 27 (06) :960-966

[4]

Li H, 1995, FUZZY SYSTEMS MATH

[5]

Rea J R, 2007, AIAA PAPER, P6424

[6]

Su W, 1996, STAT RES, P5

[7]

Tang Jin-zu, 2012, Fire Control and Command Control, V37, P120

[8]

Wang P.Z., 1985, Fuzzy sets and random sets shadow

[9]

WENDELSDORF KV, 2009, TACTICAL MISSILE TEC, V5

← 1 →