Flight Dynamic Models

Part of the Control Engineering book series (CONTRENGIN)


To present the basic flight dynamics modeling approach applicable to aircraft, rockets, and spacecraft. To derive the equations of motion for typical flight dynamic systems. To describe the sensors used in flight control systems.


Aerodynamic Force Inertial Measurement Unit Inertial Navigation System Sideslip Angle Flight Vehicle 
These keywords were added by machine and not by the authors. This process is experimental and the keywords may be updated as the learning algorithm improves.

Copyright information

© Springer Science+Business Media, LLC 2011

Authors and Affiliations

  1. 1.Department of Aerospace EngineeringIndian Institute of TechnologyKanpurIndia

Personalised recommendations