A A 516
Stability and Control of Flight Vehicles
Static and dynamic stability and control of flight vehicles in the atmosphere. Determination of stability derivatives. Effects of stability derivatives on flight characteristics. Flight dynamic model. Responses to control inputs and external disturbances. Handling qualities. Control system components, sensor characteristics. Stability augmentation systems. Prerequisite: A A 447. Offered: W.
Sources
- Course catalogue ↗Current public catalogue; retrieved 2026-11-05