Design of Air Traffic Control Operation System
Journal Title: INCAS BULLETIN - Year 2017, Vol 9, Issue 3
Abstract
This paper presents a numerical simulation for a different aircraft, based on the specific aircraft data that can be incorporated in the model and the equations of motions which can be consequently solved. The aircraft flight design involves various technical steps and requires the use of sophisticated software having modeling and simulation capabilities. Within the flight simulation model, the aerodynamic model can be regarded as the most complex and most important. With appropriate aerodynamic modeling the aerodynamic forces and moments acting on the aircraft's center of gravity can be numerically solved with accuracy. These forces and moments are further used to solve the equations of motion. The development of control and computing technology makes it possible for advanced flight control strategy. The advanced control techniques tend to make the control design and their implementation much more complicated with more control loops or channels; in this line, the autopilot of modern aircrafts includes a variety of automatic control systems that aid and support the flight navigation, flight management, and perform the enhancing and/or augmenting of the stability characteristics of the airplane. Therefore in this context it is very important to choose the dynamic that will satisfy the performance and robustness specifications.
Authors and Affiliations
Gabriela STROE, Irina-Carmen ANDREI, Tiberiu Adrian SALAORU
Keywords
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- EP ID EP294044
- DOI 10.13111/2066-8201.2017.9.3.9
- Views 114
- Downloads 0
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