TEST BANK FOR Fundamentals of Dynamics and Control of Space Systems By Krishna Dev Kumar Converted

2.1 The coordinate frames used in studying the dynamics of a spacecraft are as follows: a) Inertial reference frame, b) Orbital reference frame, c) Perifocal reference frame, c) Satellite body-fixed reference frame. 2.2 The inertial frames are those coordinate frames that are nonrotating and nonaccelerating frames. The inertial frames are relevant because in applying the Newton’s second law of motion ~F = m d~V dt (2.1) to derive the equation of motion of a system, the velocity ~V...