ENAE 642
Atmospheric Flight Control
Exposure to flight guidance and control. Draws heavily from vehicle dynamics as well as feedback theory, and careful treatment of the non-linear aspects of the problem is critical. Conventional sythesis techniques are stressed, although modern methods are not ignored. Multivariable system analysis is included, along with flight-control design objectives and hardware limitations. Emphasis on aircraft and missiles.
Prerequisites & course information
Prerequisite: ENAE403 and ENAE432 ; or students who have taken courses with comparable content may contact the department.
Sources
- Course catalogue ↗2026-2027