Model predictive control with output feedback for a deorbiting electrodynamic tether system

Hao Wen; Zheng H. Zhu; Dongping Jin; Haiyan Hu

doi:10.2514/1.G000535

Model predictive control with output feedback for a deorbiting electrodynamic tether system

Hao Wen^*, Zheng H. Zhu, Dongping Jin, Haiyan Hu

^*Corresponding author for this work

Research output: Contribution to journal › Article › peer-review

41 Citations (Scopus)

Abstract

A study is devoted to the rapid and stable deorbit of an electrodynamic tether (EDT) system in an inclined orbit via the output feedback control of the electric current flowing in the EDT. The proposed controller is designed on a basis of the model predictive control (MPC) method so as to optimize the deorbiting performance while accounting for the system constraints and nonlinear dynamics. The orbital motions of the system are described using the modified equinoctial (ME) elements, which are nonsingular for all trajectories with inclination below 180 degrees instead of the classical Keplerian orbital elements.

Original language	English
Pages (from-to)	2451-2456
Number of pages	6
Journal	Journal of Guidance, Control, and Dynamics
Volume	39
Issue number	10
DOIs	https://doi.org/10.2514/1.G000535
Publication status	Published - 2016
Externally published	Yes

Access to Document

10.2514/1.G000535

Cite this

@article{38b5d80e66344265a63d2f0033f16fad,

title = "Model predictive control with output feedback for a deorbiting electrodynamic tether system",

abstract = "A study is devoted to the rapid and stable deorbit of an electrodynamic tether (EDT) system in an inclined orbit via the output feedback control of the electric current flowing in the EDT. The proposed controller is designed on a basis of the model predictive control (MPC) method so as to optimize the deorbiting performance while accounting for the system constraints and nonlinear dynamics. The orbital motions of the system are described using the modified equinoctial (ME) elements, which are nonsingular for all trajectories with inclination below 180 degrees instead of the classical Keplerian orbital elements.",

author = "Hao Wen and Zhu, {Zheng H.} and Dongping Jin and Haiyan Hu",

year = "2016",

doi = "10.2514/1.G000535",

language = "English",

volume = "39",

pages = "2451--2456",

journal = "Journal of Guidance, Control, and Dynamics",

issn = "0731-5090",

publisher = "American Institute of Aeronautics and Astronautics Inc. (AIAA)",

number = "10",

}

TY - JOUR

T1 - Model predictive control with output feedback for a deorbiting electrodynamic tether system

AU - Wen, Hao

AU - Zhu, Zheng H.

AU - Jin, Dongping

AU - Hu, Haiyan

PY - 2016

Y1 - 2016

N2 - A study is devoted to the rapid and stable deorbit of an electrodynamic tether (EDT) system in an inclined orbit via the output feedback control of the electric current flowing in the EDT. The proposed controller is designed on a basis of the model predictive control (MPC) method so as to optimize the deorbiting performance while accounting for the system constraints and nonlinear dynamics. The orbital motions of the system are described using the modified equinoctial (ME) elements, which are nonsingular for all trajectories with inclination below 180 degrees instead of the classical Keplerian orbital elements.

AB - A study is devoted to the rapid and stable deorbit of an electrodynamic tether (EDT) system in an inclined orbit via the output feedback control of the electric current flowing in the EDT. The proposed controller is designed on a basis of the model predictive control (MPC) method so as to optimize the deorbiting performance while accounting for the system constraints and nonlinear dynamics. The orbital motions of the system are described using the modified equinoctial (ME) elements, which are nonsingular for all trajectories with inclination below 180 degrees instead of the classical Keplerian orbital elements.

UR - http://www.scopus.com/inward/record.url?scp=84988703533&partnerID=8YFLogxK

U2 - 10.2514/1.G000535

DO - 10.2514/1.G000535

M3 - Article

AN - SCOPUS:84988703533

SN - 0731-5090

VL - 39

SP - 2451

EP - 2456

JO - Journal of Guidance, Control, and Dynamics

JF - Journal of Guidance, Control, and Dynamics

IS - 10

ER -

Model predictive control with output feedback for a deorbiting electrodynamic tether system

Abstract

Access to Document

Other files and links

Fingerprint

Cite this