Filtering solution to relative attitude determination problem using multiple constraints

Richard Linares; John L. Crassidis; Yang Cheng

Filtering solution to relative attitude determination problem using multiple constraints

Richard Linares
, John L. Crassidis
, Yang Cheng

Department of Mechanical and Aerospace Engineering

SUNY Buffalo
Mississippi State University

Research output: Chapter in Book/Report/Conference proceeding › Conference contribution › peer-review

1 Scopus citations

Abstract

In this paper a filtering solution for the relative attitude and relative position of a formation of two spacecraft with multiple constraints is shown. The solution for the relative attitude and position between the two spacecraft is obtained only using line-of-sight measurements between them and a common (unknown) object observed by both spacecraft. The constraint used in the solution is a triangle constraint on the vector observations. This approach is extended to multiple objects by applying this constraint for each common object. Simulation runs to study the performance of the approach are shown.

Original language	English
Title of host publication	Spaceflight Mechanics 2012 - Advances in the Astronautical Sciences
Subtitle of host publication	Proceedings of the 22nd AAS/AIAA Space Flight Mechanics Meeting
Pages	235-254
Number of pages	20
State	Published - 2012
Event	22nd AAS/AIAA Space Flight Mechanics Meeting - Charleston, SC, United States Duration: Feb 2 2012 → Feb 2 2012

Publication series

Name	Advances in the Astronautical Sciences
Volume	143
ISSN (Print)	0065-3438

Conference

Conference	22nd AAS/AIAA Space Flight Mechanics Meeting
Country/Territory	United States
City	Charleston, SC
Period	02/2/12 → 02/2/12

Cite this

@inproceedings{d0ebf291387c4f7f801168af77fc1672,

title = "Filtering solution to relative attitude determination problem using multiple constraints",

abstract = "In this paper a filtering solution for the relative attitude and relative position of a formation of two spacecraft with multiple constraints is shown. The solution for the relative attitude and position between the two spacecraft is obtained only using line-of-sight measurements between them and a common (unknown) object observed by both spacecraft. The constraint used in the solution is a triangle constraint on the vector observations. This approach is extended to multiple objects by applying this constraint for each common object. Simulation runs to study the performance of the approach are shown.",

author = "Richard Linares and Crassidis, \{John L.\} and Yang Cheng",

year = "2012",

language = "English",

isbn = "9780877035817",

series = "Advances in the Astronautical Sciences",

pages = "235--254",

booktitle = "Spaceflight Mechanics 2012 - Advances in the Astronautical Sciences",

note = "22nd AAS/AIAA Space Flight Mechanics Meeting ; Conference date: 02-02-2012 Through 02-02-2012",

}

Linares, R, Crassidis, JL & Cheng, Y 2012, Filtering solution to relative attitude determination problem using multiple constraints. in Spaceflight Mechanics 2012 - Advances in the Astronautical Sciences: Proceedings of the 22nd AAS/AIAA Space Flight Mechanics Meeting. Advances in the Astronautical Sciences, vol. 143, pp. 235-254, 22nd AAS/AIAA Space Flight Mechanics Meeting, Charleston, SC, United States, 02/2/12.

Filtering solution to relative attitude determination problem using multiple constraints. / Linares, Richard; Crassidis, John L.; Cheng, Yang.
Spaceflight Mechanics 2012 - Advances in the Astronautical Sciences: Proceedings of the 22nd AAS/AIAA Space Flight Mechanics Meeting. 2012. p. 235-254 (Advances in the Astronautical Sciences; Vol. 143).

Research output: Chapter in Book/Report/Conference proceeding › Conference contribution › peer-review

TY - GEN

T1 - Filtering solution to relative attitude determination problem using multiple constraints

AU - Linares, Richard

AU - Crassidis, John L.

AU - Cheng, Yang

PY - 2012

Y1 - 2012

N2 - In this paper a filtering solution for the relative attitude and relative position of a formation of two spacecraft with multiple constraints is shown. The solution for the relative attitude and position between the two spacecraft is obtained only using line-of-sight measurements between them and a common (unknown) object observed by both spacecraft. The constraint used in the solution is a triangle constraint on the vector observations. This approach is extended to multiple objects by applying this constraint for each common object. Simulation runs to study the performance of the approach are shown.

AB - In this paper a filtering solution for the relative attitude and relative position of a formation of two spacecraft with multiple constraints is shown. The solution for the relative attitude and position between the two spacecraft is obtained only using line-of-sight measurements between them and a common (unknown) object observed by both spacecraft. The constraint used in the solution is a triangle constraint on the vector observations. This approach is extended to multiple objects by applying this constraint for each common object. Simulation runs to study the performance of the approach are shown.

UR - https://www.scopus.com/pages/publications/84879371799

M3 - Conference contribution

AN - SCOPUS:84879371799

SN - 9780877035817

T3 - Advances in the Astronautical Sciences

SP - 235

EP - 254

BT - Spaceflight Mechanics 2012 - Advances in the Astronautical Sciences

T2 - 22nd AAS/AIAA Space Flight Mechanics Meeting

Y2 - 2 February 2012 through 2 February 2012

ER -

Filtering solution to relative attitude determination problem using multiple constraints

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