C. J. Damaren    UTIAS   416-667-7704   damaren@utias.utoronto.ca

Teaching Assistant

Stephen Takacs    UTIAS                  takacs@utias.utoronto.ca

Lectures

Mon, 2-4pm 
Tue, 9-11am 

The primary reference is the lecturer's notes.
Spacecraft Attitude Dynamics, P. C. Hughes, John Wiley 1986.
Spaceflight Dynamics, W. E. Wiesel, McGraw-Hill, 1989.
Orbital Mechanics, V. A. Chobotov, AIAA Education Series, 1991.
Fundamentals of Astrodynamics, R. R. Bate, D. D. Mueller, J. E. White, Dover 1971.
Modern Spacecraft Dynamics and Control, M. H. Kaplan, John Wiley, 1976.
Introductory Orbital Dynamics, F. P. J. Rimrott, Vieweg, 1989. 
Spacecraft Attitude Determination and Control, J. R. Wertz, Kluwer, 1978.
Design of Geosynchronous Spacecraft, B. N. Agrawal, Prentice-Hall, 1986.

No.	Topic	Notes

A       Rigid Body Kinematics and Dynamics
1       Kinematics of a Rigid Body notes1.pdf
2	Rigid Body Dynamics        notes2.pdf
         
B       Orbital Dynamics and Control
3       The Two Body Problem       
4	Orbital Perturbations	  
5	Orbital Maneuvers         
6	Interplanetary Trajectories                                                   
7	The Restricted Three Body Problem
  
C	Attitude Dynamics and Control    
8	Torque-Free Motion                 
9	Spin-Stabilization                 
10	Dual-Spin Stabilization           
11      Disturbance Torques                
12      Gravity-Gradient Stabilization    
13      Spin Stabilization Revisited       
14      Active Spacecraft Attitude Control 
15	Bias-Momentum Stabilization        
  

Assignments      15%
Midterm Test     25%
Final Examinaton 60%