ECE 5230: Spacecraft Systems Engineering
Spacecraft communications, telemetry systems, and command and data handling. Introduction to astrodynamics and orbit design. Electrical power generation and storage. Spacecraft subsystems (e.g., guidance, navigation, and control).
Prerequisite/Restriction: MATH 2270, MATH 2280, and student must be in the Professional Engineering Program or have Graduate Standing
Semester(s) Traditionally Offered: FALL
Course Instructor: Lucas Anderson
Textbook: Spacecraft Systems Engineering, 3rd or 4th edition (ISBN - 0-470-85102-3 or 0-471-61951-5)