Fundamentals of optimal control theory and calculus of variations. Application of this theory to aerospace engineering problems, including mission design problems and a wide range of space maneuvers. A-F only. Junior standing or higher. Pre: grade of C or better in all of the following: 271; 375; MATH 244 or MATH 253A; MATH 302 or MATH 307; EE 160 or ICS 111.