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ECE 5230: Spacecraft Systems Engineering

3 Credits
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 Syllabus

Course Instructor: Charles Swenson

Textbook: Spacecraft Systems Engineering, 3rd or 4th edition (ISBN - 0-470-85102-3 or 0-471-61951-5)