À¦°óSMÉçÇø

MECH 542 Spacecraft Dynamics (3 credits)

Note: This is the 2014–2015 edition of the eCalendar. Update the year in your browser's URL bar for the most recent version of this page, or click here to jump to the newest eCalendar.

Offered by: Mechanical Engineering (Faculty of Engineering)

Overview

Mechanical Engineering : Review of central force motion; Hohmann and other coplanar transfers, rotation of the orbital plane, patched conic method. Orbital perturbations due to the earth's oblateness, solar-lunar attraction, solar radiation pressure and atmospheric drag. Attitude dynamics of a rigid spacecraft; attitude stabilization and control; attitude manoeuvers; large space structures.

Terms: Fall 2014

Instructors: Jalali Mashayekhi, Mohammad (Fall)

Back to top