Aircraft Dynamic Stability & Design of Stability Augmentation System
- 0
- 8 weeks long
- Swayam
- English
Course Overview
This course is designed to understand aspects of advance dynamic stability of an airplane. This course will also help in creating a background to design an airplane from stability and control aspects.
Course Circullum
Week 1:
Introduction to dynamic stability
Introduction to dynamic stability
First and second order system
First and second order system
Solution of second order system using Laplace transform
Week 2:
Physical interpretation of natural and damped frequencies damping ratio time to half and time to double
Physical interpretation of natural and damped frequencies damping ratio time to half and time to double
Physical interpretation of natural and damped frequencies damping ratio time to half and time to double
6dof equations motion of aircraft
6dof equations motion of aircraft
Week 3:
Euler angles
Euler angles
Development of longitudinal small perturbed equations of motion
Development of longitudinal small perturbed equations of motion
Development of longitudinal small perturbed equations of motion
Week 4:
Dimensional derivatives
Dimensional derivatives
Roots
short period and long period mode
short period and long period mode
Week 5:
Design of SAS for longitudinal mode
Design of SAS for longitudinal mode
Transfer function and longitudinal mode shapes
Lateral directional perturbed equations of motion
Lateral directional perturbed equations of motion
Week 6:
Dimensional derivatives lateral
Dimensional derivatives lateral
Roots lateral
Spiral roll and dutch roll mode
Spiral roll and dutch roll mode
Week 7:
Transfer function Lateral
Transfer function Lateral
Design of SAS For lateral
Design of SAS For lateral
Design of SAS For lateral
Week 8:
Mode shape
Mode shape
Mode shape
Inertial Sensors
Inertial Sensors
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This Course Include:
Week 1:
Introduction to dynamic stability
Introduction to dynamic stability
First and second order system
First and second order system
Solution of second order system using Laplace transform
Week 2:
Physical interpretation of natural and damped frequencies damping ratio time to half and time to double
Physical interpretation of natural and damped frequencies damping ratio time to half and time to double
Physical interpretation of natural and damped frequencies damping ratio time to half and time to double
6dof equations motion of aircraft
6dof equations motion of aircraft
Week 3:
Euler angles
Euler angles
Development of longitudinal small perturbed equations of motion
Development of longitudinal small perturbed equations of motion
Development of longitudinal small perturbed equations of motion
Week 4:
Dimensional derivatives
Dimensional derivatives
Roots
short period and long period mode
short period and long period mode
Week 5:
Design of SAS for longitudinal mode
Design of SAS for longitudinal mode
Transfer function and longitudinal mode shapes
Lateral directional perturbed equations of motion
Lateral directional perturbed equations of motion
Week 6:
Dimensional derivatives lateral
Dimensional derivatives lateral
Roots lateral
Spiral roll and dutch roll mode
Spiral roll and dutch roll mode
Week 7:
Transfer function Lateral
Transfer function Lateral
Design of SAS For lateral
Design of SAS For lateral
Design of SAS For lateral
Week 8:
Mode shape
Mode shape
Mode shape
Inertial Sensors
Inertial Sensors
- Provider:Swayam
- Certificate:Certificate Available
- Language:English
- Duration:8 weeks long
- Language CC: