On-off control of flexible spacecraft with specified fuel usage

William Singhose; Tarunraj Singh; Warren Seering

doi:10.1109/acc.1997.609038

On-off control of flexible spacecraft with specified fuel usage

William Singhose
, Tarunraj Singh
, Warren Seering

Department of Mechanical and Aerospace Engineering

Massachusetts Institute of Technology

Research output: Contribution to journal › Conference article › peer-review

13 Scopus citations

Abstract

A method for generating on-off command profiles for flexible systems is presented. The command profiles move a system without residual vibration while using a specified amount of actuator fuel. Robustness to modeling errors can be incorporated into the design of the command signals. Techniques are presented which facilitate implementation and indicate prudent choices for the amount of fuel to be used. The method is compared to other command generation techniques that balance fuel usage and slew time.

Original language	English
Pages (from-to)	2308-2312
Number of pages	5
Journal	Proceedings of the American Control Conference
Volume	4
DOIs	https://doi.org/10.1109/acc.1997.609038
State	Published - 1997
Event	Proceedings of the 1997 American Control Conference. Part 3 (of 6) - Albuquerque, NM, USA Duration: Jun 4 1997 → Jun 6 1997

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10.1109/acc.1997.609038

Cite this

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title = "On-off control of flexible spacecraft with specified fuel usage",

abstract = "A method for generating on-off command profiles for flexible systems is presented. The command profiles move a system without residual vibration while using a specified amount of actuator fuel. Robustness to modeling errors can be incorporated into the design of the command signals. Techniques are presented which facilitate implementation and indicate prudent choices for the amount of fuel to be used. The method is compared to other command generation techniques that balance fuel usage and slew time.",

author = "William Singhose and Tarunraj Singh and Warren Seering",

year = "1997",

doi = "10.1109/acc.1997.609038",

language = "English",

volume = "4",

pages = "2308--2312",

journal = "Proceedings of the American Control Conference",

issn = "0743-1619",

publisher = "Institute of Electrical and Electronics Engineers Inc.",

note = "Proceedings of the 1997 American Control Conference. Part 3 (of 6) ; Conference date: 04-06-1997 Through 06-06-1997",

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TY - JOUR

T1 - On-off control of flexible spacecraft with specified fuel usage

AU - Singhose, William

AU - Singh, Tarunraj

AU - Seering, Warren

PY - 1997

Y1 - 1997

N2 - A method for generating on-off command profiles for flexible systems is presented. The command profiles move a system without residual vibration while using a specified amount of actuator fuel. Robustness to modeling errors can be incorporated into the design of the command signals. Techniques are presented which facilitate implementation and indicate prudent choices for the amount of fuel to be used. The method is compared to other command generation techniques that balance fuel usage and slew time.

AB - A method for generating on-off command profiles for flexible systems is presented. The command profiles move a system without residual vibration while using a specified amount of actuator fuel. Robustness to modeling errors can be incorporated into the design of the command signals. Techniques are presented which facilitate implementation and indicate prudent choices for the amount of fuel to be used. The method is compared to other command generation techniques that balance fuel usage and slew time.

UR - https://www.scopus.com/pages/publications/0030693510

U2 - 10.1109/acc.1997.609038

DO - 10.1109/acc.1997.609038

M3 - Conference article

AN - SCOPUS:0030693510

SN - 0743-1619

VL - 4

SP - 2308

EP - 2312

JO - Proceedings of the American Control Conference

JF - Proceedings of the American Control Conference

T2 - Proceedings of the 1997 American Control Conference. Part 3 (of 6)

Y2 - 4 June 1997 through 6 June 1997

ER -

On-off control of flexible spacecraft with specified fuel usage

Abstract

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