Investigation of the crossed flexure pivot and the dynamics of the momentum management system, spacecraft control component and the dynamically tuned gyroscope.

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Creator: 

Cain, Jeffrey S.

Date: 

1999

Subject: 

Space Vehicles -- Attitude Control Systems
Gyroscopes
Hamilton-jacobi Equations -- Computer Simulation
Lagrange Equations -- Computer Simulation
Kinematics -- Computer Simulation

Language: 

English

Publisher: 

Carleton University

Identifier: 

Proquest Record
Library Catalogue Record
https://doi.org/10.22215/etd/1999-04206

Thesis Degree Name: 

Doctor of Philosophy: 
Ph.D.

Thesis Degree Level: 

Doctoral

Thesis Degree Discipline: 

Engineering, Mechanical and Aerospace

Parent Collection: 

Theses and Dissertations

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