Description
Name of Notes : – Flight dynamics II – Airplane stability and control Lecture Note
Introduction
Flight dynamics deals principally with the response of aerospace vehicles to perturbations in their flight environments and to control inputs. In order to understand this response, it is necessary to characterize the aerodynamic and propulsive forces and moments acting on the vehicle, and the dependence of these forces and moments on the flight variables, including airspeed and vehicle orientation. These notes provide an introduction to the engineering science of flight dynamics, focusing primarily of aspects of stability and control. The notes contain a simplified summary of important results from aerodynamics that can be used to characterize the forcing functions, a description of static stability for the longitudinal problem, and an introduction to the dynamics and control of both, longitudinal and lateral/directional problems, including some aspects of feedback control.
Modules / Lectures
- Module 1 – Chapter 1 – Introduction
- Module 2 – Chapter 2 – Longitudinal stick-fixed static stability and control
- Module 3 – Chapter 3 – Longitudinal stick-free static stability and control
- Module 4 – Chapter 4 – Longitudinal static stability & control – Effect of acceleration
- Module 5 – Chapter 5 – Directional static stability and control
- Module 6 – Chapter 6 – Lateral static stability and control
- Module 7 – Chapter 7 – Dynamic stability analysis – I – Equations of motion and estimation of stabil
- Module 8 – Chapter 8 – Dynamic stability analysis – II – Longitudinal motion
- Module 9 – Chapter 9 – Dynamic stability analysis – III – Lateral motion
- Module 10 – Chapter 10 – Miscellaneous topics
- Module-11-Appendix-C Drag polar,stability derivatives and characteristic roots of a jet airplane
- Module 12 – Sample Question paper and answers
Reviews
There are no reviews yet