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Aircraft Stability and Control

IIT Kanpur, , Prof. Dr. A.K. Ghosh

Updated On 02 Feb, 19

Overview

Intended Audience:

Includes

Lecture 55: Lateral-Directional Motion

4.1 ( 11 )

Lecture Details

Course Details

COURSE LAYOUT

Week 1: Overview of aerodynamics and atmosphere, Wing stall and maximum lift coefficient,Wing aerodynamic center & pitching moment, Introduction to static and dynamic stability. 

Week 2: Introduction to static and dynamic stability, Wing contribution, Tail contribution, Canard and fuselage contribution.     

Week 3: Power plant contribution & its effect on NP, Stick fixed neutral point, Static margin, Stick fixed : maneuvering point.   

Week 4: Elevator effectiveness, Elevator angle of trim, Flight measurement of Xnp, Elevator hinge moment, Stick forces (trim tab & stick force gradient),     

Week 5: Stick free neutral point, Stick free : maneuvering point, Roll stability and roll control, Yaw stability and yaw control.     

Week 6: Newtons second law of rigid dynamics, Axes system and relevant transforms, Angular motion equations.     

Week 7: Aerodynamic forces, Gravitational and thrust forces, Linearized equations of motion, 

Week 8: Force and moment derivatives, Force and moment derivatives, Contribution of aircraft components to aerodynamic derivatives, Linear model.     

Week 9: Short period approximation,Long period approximation, Pure pitching motion, Flying and handling qualities.     

Week 10: Linearized lateral dynamics.Lateral motion :Linearized coupled motion, Roll approximation, Spiral approximation.     

Week 11: Dutch roll approximation. Pure rolling. Pure yawing, Inertia coupling.     

Week 12: Stability augmentation system: Longitudinal, Stability augmentation system: Lateral.     


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Comments
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Sam

Excellent course helped me understand topic that i couldn't while attendinfg my college.

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Dembe

Great course. Thank you very much.

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