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

It appears your Web browser is not configured to display PDF files. Download adobe Acrobat or click here to download the PDF file.

Click here to download the PDF file.

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

Thesis Degree Name: 

Doctor of Philosophy: 
Ph.D.

Thesis Degree Level: 

Doctoral

Thesis Degree Discipline: 

Engineering, Mechanical and Aerospace

Parent Collection: 

Theses and Dissertations

Items in CURVE are protected by copyright, with all rights reserved, unless otherwise indicated. They are made available with permission from the author(s).