SNS406 Spacecraft Attitude Dynamics and Control Lec 1: Intro

To provide instructions for the entire mission in a single load

To manage the spacecraft's position and attitude throughout all flight phases (correct)

To separate mission segments due to memory limitations

To test programmed flight segments before loading them into the system

To accommodate the memory limitations of the General Purpose Computers (correct)

To ensure redundancy in case of system failures

To optimize the performance of the guidance and control algorithms

To allow for software updates between mission segments

Control Subsystem

Navigation Subsystem

All subsystems contribute equally

Guidance Subsystem (correct)

<p>To monitor and report the current spacecraft position and attitude</p> Signup and view all the answers

<p>Control Subsystem</p> Signup and view all the answers

<p>They vary depending on the flight phase</p> Signup and view all the answers