QuickBird-DS-QB
GN/MAE155A1 Introduction to Attitude Control Systems MAE 155A.
Spacecraft Structure Requirements –Mass, Strength, Stiffness, Cleanliness (Particulate/Magnetic) Constraints –Fields of view (instruments, thrusters, motors)
Spacecraft Structure
Introduction to Attitude Control Systems
“CLIC MDI Meeting” on 27/01/2012
