Decoupling control for airspeed and flight path angle using an improved total energy control algorithm

Zhang Qingzhen; Gao Chen; Ma Wentao; Ren Zhang

doi:10.1109/ISSCAA.2008.4776262

Decoupling control for airspeed and flight path angle using an improved total energy control algorithm

Zhang Qingzhen^*
, Gao Chen
, Ma Wentao
, Ren Zhang

^*Corresponding author for this work

School of Automation Science and Electrical Engineering

Beihang University

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

Abstract

An improved core algorithm is proposed for "Total Energy Control System"(TECS), which diminishes the response oscillations caused by the cooperation error between aircraft total energy and its distribution. The construction of a feedback loop based on energy cooperation error to enhance decoupling performance for airspeed and flight path angle is the key step in the proposed approach. Based on the suggested method the TECS controller is synthesized for a linearized longitudinal axis aircraft model. Simulation results indicate that the cooperation error feedback loop can effectively reduce system response oscillations and achieves superior performance.

Original language	English
DOIs	https://doi.org/10.1109/ISSCAA.2008.4776262
State	Published - 2008
Event	2008 2nd International Symposium on Systems and Control in Aerospace and Astronautics, ISSCAA 2008 - Shenzhen, China Duration: 10 Dec 2008 → 12 Dec 2008

Conference

Conference	2008 2nd International Symposium on Systems and Control in Aerospace and Astronautics, ISSCAA 2008
Country/Territory	China
City	Shenzhen
Period	10/12/08 → 12/12/08

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10.1109/ISSCAA.2008.4776262

Cite this

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title = "Decoupling control for airspeed and flight path angle using an improved total energy control algorithm",

abstract = "An improved core algorithm is proposed for {"}Total Energy Control System{"}(TECS), which diminishes the response oscillations caused by the cooperation error between aircraft total energy and its distribution. The construction of a feedback loop based on energy cooperation error to enhance decoupling performance for airspeed and flight path angle is the key step in the proposed approach. Based on the suggested method the TECS controller is synthesized for a linearized longitudinal axis aircraft model. Simulation results indicate that the cooperation error feedback loop can effectively reduce system response oscillations and achieves superior performance.",

author = "Zhang Qingzhen and Gao Chen and Ma Wentao and Ren Zhang",

year = "2008",

doi = "10.1109/ISSCAA.2008.4776262",

language = "英语",

note = "2008 2nd International Symposium on Systems and Control in Aerospace and Astronautics, ISSCAA 2008 ; Conference date: 10-12-2008 Through 12-12-2008",

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AU - Qingzhen, Zhang

AU - Chen, Gao

AU - Wentao, Ma

AU - Zhang, Ren

PY - 2008

Y1 - 2008

N2 - An improved core algorithm is proposed for "Total Energy Control System"(TECS), which diminishes the response oscillations caused by the cooperation error between aircraft total energy and its distribution. The construction of a feedback loop based on energy cooperation error to enhance decoupling performance for airspeed and flight path angle is the key step in the proposed approach. Based on the suggested method the TECS controller is synthesized for a linearized longitudinal axis aircraft model. Simulation results indicate that the cooperation error feedback loop can effectively reduce system response oscillations and achieves superior performance.

AB - An improved core algorithm is proposed for "Total Energy Control System"(TECS), which diminishes the response oscillations caused by the cooperation error between aircraft total energy and its distribution. The construction of a feedback loop based on energy cooperation error to enhance decoupling performance for airspeed and flight path angle is the key step in the proposed approach. Based on the suggested method the TECS controller is synthesized for a linearized longitudinal axis aircraft model. Simulation results indicate that the cooperation error feedback loop can effectively reduce system response oscillations and achieves superior performance.

UR - https://www.scopus.com/pages/publications/66449111880

U2 - 10.1109/ISSCAA.2008.4776262

DO - 10.1109/ISSCAA.2008.4776262

M3 - 论文

AN - SCOPUS:66449111880

T2 - 2008 2nd International Symposium on Systems and Control in Aerospace and Astronautics, ISSCAA 2008

Y2 - 10 December 2008 through 12 December 2008

ER -

Decoupling control for airspeed and flight path angle using an improved total energy control algorithm

Abstract

Conference

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