Spacecraft Dynamics

课程简介

/ Indicative Syllabus Introduction to Spacecraft Dynamics: Overview of spacecraft dynamics principles; Coordinate systems and transformations used in spacecraft dynamics; Basic concepts of rigid body dynamics and kinematics applicable to spacecraft. Spacecraft Kinematics and Dynamics: Position, velocity, and acceleration in space; Relative motion and reference frames; Forces and moments acting on spacecraft; Rotational kinematics; Dynamic differential equations of spacecraft; External torques on spacecraft. Orbit Determination and Propagation: Orbit determination techniques using ground-based and onboard sensors; Propagation of orbital elements and trajectory prediction. Attitude Dynamics and Control: Attitude representation and dynamics; Attitude control systems and stabilisation techniques. Guidance and Navigation: Principles of guidance and navigation in space; Orbit transfer manoeuvres and rendezvous operations. -- 1 of 3 -- 2 Spacecraft Formation Flying: Dynamics of multiple spacecraft formations; Control strategies for maintaining formation configurations; Mission Design and Analysis: Mission requirements and constraints; Trajectory optimisation and mission analysis techniques; Case Studies and Applications.

目标

To equip students with an understanding of theoretical and practical spacecraft dynamics from the perspective of dynamical systems, using a cohesive and integrated approach to mathematical modelling, analysis, and control of advanced space vehicles.

先修要求

/ Co-requisite/ Exclusion Nil

Teaching Pattern

Methodology The teaching and learning methods include lectures, mini-project, and homework assignments. Technical/practical examples and problems will be raised and discussed in class. Project is designed to evaluate the spacecraft dynamics. Teaching/Learning Methodology Outcomes a b c d Lecture ✓ ✓ ✓ ✓ Mini-project ✓ ✓ ✓ ✓ Homework assignments ✓ ✓ ✓ ✓