Description
Aircraft nonlinear equations of motion and their linearization; effect of stability and control derivatives on the open-loop dynamics response; autopilot design and aircraft stability and control augmentation; pilot-in-the-loop; aeroelastic effects on stability and control.
Conditions and arrangements
- Also listed as MAAJ 5151 .
Reference text in its original language
Aircraft nonlinear equations of motion and their linearization; effect of stability and control derivatives on the open-loop dynamics response; autopilot design and aircraft stability and control augmentation; pilot-in-the-loop; aeroelastic effects on stability and control.
- Also listed as MAAJ 5151 .
Sources and references
Dates and sources are retained to help you verify the information. Translations are provided to facilitate reading; the official source governs conditions and requirements.
Source reference : https://calendar.carleton.ca/grad/courses/MECH/