Modeling and control of flyable boom in aerial refueling

Songshan Yang; Yakui Gao; Zongji Chen; Weiqi Li

Modeling and control of flyable boom in aerial refueling

Songshan Yang^*
, Yakui Gao
, Zongji Chen
, Weiqi Li

^*Corresponding author for this work

School of Automation Science and Electrical Engineering

Research output: Contribution to conference › Paper › peer-review

Abstract

The concept of flyable boom was adopted in the Air-to-Air refueling system, it is obvious that refueling speed is faster than the traditional refueling hose from tanker to receiver. The flyable boom works in the intense and unstable airflow condition, not only the precise mathematical models need to be constructed, but also the stability of flyable boom is concerned during the refueling. The linear quadratic regulator flight control law was designed and it can make the flyable boom hold attitude better effectively. In nonlinear simulation of MATLAB and associated simulation condition of MATLAB and ADAMS, the good results were obtained.

Original language	English
Pages	56-60
Number of pages	5
State	Published - 2005
Event	Asian Simulation Conference 2005, ASC 2005 and the 6th International Conference on System Simulation and Scientific Computing, ICSC 2005 - Beijing, China Duration: 24 Oct 2005 → 27 Oct 2005

Conference

Conference	Asian Simulation Conference 2005, ASC 2005 and the 6th International Conference on System Simulation and Scientific Computing, ICSC 2005
Country/Territory	China
City	Beijing
Period	24/10/05 → 27/10/05

Keywords

Air-to-air
Flyable boom
LQR
Refueling

Cite this

@conference{94adecf2311849abb79595e19444b511,

title = "Modeling and control of flyable boom in aerial refueling",

abstract = "The concept of flyable boom was adopted in the Air-to-Air refueling system, it is obvious that refueling speed is faster than the traditional refueling hose from tanker to receiver. The flyable boom works in the intense and unstable airflow condition, not only the precise mathematical models need to be constructed, but also the stability of flyable boom is concerned during the refueling. The linear quadratic regulator flight control law was designed and it can make the flyable boom hold attitude better effectively. In nonlinear simulation of MATLAB and associated simulation condition of MATLAB and ADAMS, the good results were obtained.",

keywords = "Air-to-air, Flyable boom, LQR, Refueling",

author = "Songshan Yang and Yakui Gao and Zongji Chen and Weiqi Li",

year = "2005",

language = "英语",

pages = "56--60",

note = "Asian Simulation Conference 2005, ASC 2005 and the 6th International Conference on System Simulation and Scientific Computing, ICSC 2005 ; Conference date: 24-10-2005 Through 27-10-2005",

}

TY - CONF

T1 - Modeling and control of flyable boom in aerial refueling

AU - Yang, Songshan

AU - Gao, Yakui

AU - Chen, Zongji

AU - Li, Weiqi

PY - 2005

Y1 - 2005

N2 - The concept of flyable boom was adopted in the Air-to-Air refueling system, it is obvious that refueling speed is faster than the traditional refueling hose from tanker to receiver. The flyable boom works in the intense and unstable airflow condition, not only the precise mathematical models need to be constructed, but also the stability of flyable boom is concerned during the refueling. The linear quadratic regulator flight control law was designed and it can make the flyable boom hold attitude better effectively. In nonlinear simulation of MATLAB and associated simulation condition of MATLAB and ADAMS, the good results were obtained.

AB - The concept of flyable boom was adopted in the Air-to-Air refueling system, it is obvious that refueling speed is faster than the traditional refueling hose from tanker to receiver. The flyable boom works in the intense and unstable airflow condition, not only the precise mathematical models need to be constructed, but also the stability of flyable boom is concerned during the refueling. The linear quadratic regulator flight control law was designed and it can make the flyable boom hold attitude better effectively. In nonlinear simulation of MATLAB and associated simulation condition of MATLAB and ADAMS, the good results were obtained.

KW - Air-to-air

KW - Flyable boom

KW - LQR

KW - Refueling

UR - https://www.scopus.com/pages/publications/84902485941

M3 - 论文

AN - SCOPUS:84902485941

SP - 56

EP - 60

T2 - Asian Simulation Conference 2005, ASC 2005 and the 6th International Conference on System Simulation and Scientific Computing, ICSC 2005

Y2 - 24 October 2005 through 27 October 2005

ER -

Modeling and control of flyable boom in aerial refueling

Abstract

Conference

Keywords

Other files and links

Fingerprint

Cite this