| Category | Coursework | Subject | Engineering |
|---|---|---|---|
| University | University of Nottingham | Module Title | MMM2058 Aircraft Dynamics and Control |
The rolling motion of an aircraft is governed by the aileron deflection, which generates a rolling moment. The role dynamics can be approximated as a first-order or second-order system (as discussed in the lecture).
An aircraft rolling dynamics is shown in Figure 1, assuming J (m2kg)is the moment of inertia in roll dynamics; λ (Nms/rad) is the air resistant torque coefficient; δ is the disturbance torque, c(t) (Nm) is the control torque provided by aileron deflection. The required roll rate is ω_ref (rad/s).
Do You Need MMM2058 Assignment of This Question
Order Non Plagiarized AssignmentLO1 - Define and characterise the dynamic response of aircraft.
LO2 - - Represent and analyse an aerospace system in linearized form.
LO3 - Conduct practical investigations of aircraft dynamics to accurately characterise flight modes
LO4 Demonstrate understanding of control system theory when applied to aerospace-related problems.
LO5 - Use the principles of control theory to construct analyses of aerospace systems to achieve desirable response characteristics
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