JOURNAL BROWSE
Search
Advanced SearchSearch Tips
Ground Test and Evaluation of a Flight Control Systemfor Unmanned Aerial Vehicles
facebook(new window)  Pirnt(new window) E-mail(new window) Excel Download
 Title & Authors
Ground Test and Evaluation of a Flight Control Systemfor Unmanned Aerial Vehicles
Suk, Jin-Young;
  PDF(new window)
 Abstract
UAV(Unmanned Aerial Vehicle) has become one of the most popularmilitary/commercial aerial robots in the new millennium. In spite of all theadvantages that UAVs inherently have, it is not an easv job to develop a UAVbecause it requires very systematic and complete approaches in full developmentenvelop. The ground test and evaluation phase has the utmost importance in thesense that a well-developed system can be best verified on the ground. In addition,many of the aircraft crashes in the flight tests were resulted from the incompletedevelopment procedure. In this research, a verification procedure of the wholeairbome integrated system was conducted including the flight management system.An airbome flight control computer(FCC) senses the extemal environment from thepehpheral devices and sends the control signal to the actuating system using theassigned control logic and flight test strategy. A ground test station controls themission during the test while the downlink data are transferred from the flightmanagement computer using the serial communication interface. The pilot controlbox also applies additional manual actuating commands. The whole system wastested/verified on the wind-tunnel system, which gave a good pitch controlperformance with a preUspecified flight test procedure. The ground test systemguarantees the performance of fundamental functions of airbome electronic systemfor the future flight tests.
 Keywords
UAV;Ground Test and Evaluation;Flight Test;Flight ManagementSystem;Communication Interface;Pilot Box;Wind-Tunnel;AirbomeElectronic System;
 Language
English
 Cited by
 References
1.
Y. Nam and J. Ko, Application Technology of the R&D Aircraft Simulator, ICASE Journal, Vol. 3, No. 2, 1997, pp.64-77

2.
Y. Kim, M. Tahk, and J. Lee, 'A Study on Hardware-in-the-loop Simulations of a Flight Control System,' KSASS Journal, Vol. 22, No. 2, 1994, pp.81-92

3.
S. Lee, V. Povstyanoy, K. Noh, J. Park, S. Ko, ' A Study on Engineering Software Design for Aircraft Development,' Proceedings of the KSAS Annual Conference, 1999, pp. 100-104

4.
S. Yoon, 'Airplane R&D Simulator,' KSASS Journal, Vol. 30, No. 7, 2002, pp.150-162

5.
Jessica A. Woods-Vedeler, Anthony S. Pototzky, and Sherwood T. Hoadley, Actiue Load ControI During RolIing Maneuvers. NASA-TP-3455, 1994

6.
Nelson J. Groom, Simplified Anatytical Model of a Six-Degree-of-Freedom Large-Gap Magnetic Suspension System, NASA-TM-112868, 1997