Flight dynamics - introduction, Other Engineering

Assignment Help:

In the Aircraft Performance course, the aircraft was assumed to be in a steady-state (e.g. steady  cruise, climb, turn, glide), with the forces and moments balanced. The subject of Flight Dynamics is concerned with what happens when the forces and moments are not in balance. It deals with

1. The question of stability: i.e. whether the aircraft will tend to settle down to steady state following a disturbance, or whether it will depart, possibly entering dangerous flight regimes.

2. The aircraft's dynamic response to control inputs and atmospheric disturbances.  

This lecture course will build on aerodynamics, aircraft performance, mechanics and system theory to develop the theory of flight dynamics. This will be followed by a series of lectures given by Dr Shenton devoted to flight control systems.  One of the key issues considered at an early stage in Flight Dynamics is stability. Roughly speaking, this equates to the tendency of the aircraft to return to an equilibrium flight condition following a perturbation from its flight path caused by an atmospheric disturbance or pilot inputs on the controls. The nature of the aircraft's response is determined by solving the equations of motion which capture the "physics" of the system. Before considering the solutions to the dynamical equations, it is customary to consider so-called static stability. This deals with the question of whether the forces and moments generated by disturbances tend to be stabilizing or destabilizing.


Related Discussions:- Flight dynamics - introduction

Mass Transfer, construction and working of counter flow tray

construction and working of counter flow tray

Electronic engine control systems - aircraft engine, Electronic engine cont...

Electronic engine control systems : Advances in gas turbine technology have demanded more precise control of engine parameters than can be provided by hydromechanical fuel cont

Aviation legislation - aircraft weight and balance, AIRCRAFT WEIGHT AND BAL...

AIRCRAFT WEIGHT AND BALANCE - Reference BCAR A5-4 or JAR-25.23 -29 After an aircraft has been constructed, painted and can be said to be ‘representative of its true empty (or

Principles of jet propulsion, Principles of Jet Propulsion: Newton 's...

Principles of Jet Propulsion: Newton 's Laws of Motion. To understand the basic principles of jet propulsion it is necessary to understand the practical application of Sir I

Difference between elastic and plastic deformation, Q. State difference bet...

Q. State difference between elastic and plastic deformation. Ans. Elastic deformation: Elastic deformation is that the part of the deformed material, when the applied load is

Principles of suveying, the true length of a line is known to be 500m.the ...

the true length of a line is known to be 500m.the line was again measured with a 20m tape and found to be 502m,what is the correct length of the 20m tape.

Components of amplifier, Expertsmind.com brings you unique solution in el...

Expertsmind.com brings you unique solution in electrical engineering RESISTORS: Resistors are designed to drop the amount of voltage going through them, this allow

Fuel control in aircraft engine, Fuel control in Aircraft Engine: ...

Fuel control in Aircraft Engine: The basic fuel system is comprised of a fuel pump that receives low-pressure fuel from the aircraft fuel tank via a low pressure fuel valv

Write Your Message!

Captcha
Free Assignment Quote

Assured A++ Grade

Get guaranteed satisfaction & time on delivery in every assignment order you paid with us! We ensure premium quality solution document along with free turntin report!

All rights reserved! Copyrights ©2019-2020 ExpertsMind IT Educational Pvt Ltd