Affiliation:
1. First Aeronautic Institute of Air Force
Abstract
This paper describes a system for evaluating flight of fixed-wing aircraft. During the flight of an aircraft, flight parameters are obtained and transmitted to the ground station by means of wireless communication. These flight data are received by the ground station and are calculated so as to get the input of flight gear, by internet interfaces flight gear can simulate the real-time state of the aircraft on the ground. The system can be used to evaluate the flight performance of a fixed-wing aircraft.
Publisher
Trans Tech Publications, Ltd.
Reference5 articles.
1. J. H. Chen, S. C. Lee, D. B. Debra. Gyroscope Free Strapdown Inertial Measurement Unit by Six Linear Accelerometers, Journal of Guidance, Control, and Dynamics, vol. 17, no. 2, 1994, pp.286-290.
2. T. H. Van Pelt and D. S. Bernstein. Least Squares Identication Using μ-Markov Parameterizations, Proc. IEEE Conf. Decision and Control, December (1998).
3. R.W. Deters, G. A. Dimock, M. S. Selig, Icing Encounter Flight Simulator with an Integrated Smart Icing System, AIAA Modeling and Simulation Technologies Conference, AIAA Paper 2002-4599, Monterey, CA, August (2002).
4. G. A. Dimock, R.W. Deters, Selig, M.S., Icing Scenarios with the Icing Encounter Flight Simulator, AIAA 41th Aerospace Sciences Meeting, AIAA Paper 2003-0023, Reno, NV, January (2003).
5. Berndt, Jon S, JSBSim: An Open Source Flight Dynamics Model in C++, AIAA Modeling and Simulation Technologies Conference and Exhibil, AIAA Paper 2004-4923, Providence, RI, August (2004).