Tytuł artykułu
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Abstrakty
The problem of manual but automation-aided controllers is very important for designers of today's equipment. Interactions of human with controllers must be properly solved and, besides design of control algorithms, the proper interfaces (information interfaces - from system to human and command interfaces - from human to system) are condition for successful operation. In the last years interest of researchers in active command interfaces (control sticks, levers), which can join both functions, has increased. In the paper, the analysis of different manual control system structures with different augmentation systems is presented. The effect of this analysis is a new control structure. The next problem which must be solved for implementation of active command interfaces is how to form its characteristics. Analysis of the controlled process responses (here, aircraft flight state) and state shows possibility of using information about aircraft state for the purpose of distinguishing some areas in the process state space and forming the force accordingly. The responses are obtained during simulation experiments. The results of simulations show proper and incorrect command depending on the flight condition and the force characteristics can be formed accordingly.
Słowa kluczowe
Czasopismo
Rocznik
Tom
Strony
67--75
Opis fizyczny
Bibliogr. 14 poz., wykr.
Twórcy
autor
- Rzeszów University of Technology, ul. W. Pola 2, 35-959 Rzeszów, Poland, jp@prz.edu.pl
Bibliografia
- [1] Cieciński P., Pieniążek J., Aircraft modelling for the control system synthesis, ML-XI Mechanika w Lotnictwie, 2004, pp. 287-300, (in Polish).
- [2] Hanke D., Herbst C., Active sidestick technology - a means for improving situational awareness, Aerospace Science and Technology, Vol. 3, 1999, pp. 525-532.
- [3] Inagaki T., Automation and the cost of autority, Int. J. of Industrial Ergonomics, Vol. 31, 2003, pp. 169-174.
- [4] McRuer D., Graham D., A Flight Control Century: Triumphs of the Systems Approach, Journal of Guidance, Control, and Dynamics, Vol. 27, No. 2, 2004, pp. 161-173.
- [5] Mulder M, Veldhuijzen A., van Paassen R., Bennani S., Fly-by-wire and Tunnel-in-the-Sky Displays: Towards a Task-Oriented Control/Display System, Proc. AIAA Guidance, Navigation, and Control Conference and Exhibit, AIAA 2002-4928, 2002.
- [6] Mulder M., Veldhuijzen A., van Paassen M.M., Mulder J.A., Integrating Fly-by-Wire Controls with Perspective Flight-Path Displays, Journal of Guidance, Control, and Dynamics, Vol. 28, No. 6, 2005, pp. 1263-1274.
- [7] Painter J.H., Valasek J., Ward D.T., Integrating the Evolving Modern Cockpit, Proc. AIAA Guidance, Navigation, and Control Conference and Exhibit, AIAA 2001-4175, 2001.
- [8] Pieniążek J., Re-configurable control system for autonomous unmanned aircraft, Proc. 7th Symp. Robot Control, SYROCO’03, Wrocław University of Technology, Vol. 1, 2003, pp. 353-358.
- [9] Rogers R., Pilot Authority and Aircraft Protections, Air Line Pilots Association, 1999.
- [10] Rong J., Ding Y., Valasek J., Cockpit System Design for General Aviation Free Flight Using a Cognitive Engineering Approach, Proc. AIAA Guidance, Navigation, and Control Conference and Exhibit, AIAA 2003-5774, 2003.
- [11] De Stigter S., Mulder M., van Paassen M.M., Design and Evaluation of a Haptic Flight Director, Journal of Guidance, Control, and Dynamics, Vol. 30, No. 1, 2007, pp. 35-46.
- [12] Tomczyk A., A proposal of handling qualities shaping for general aviation aircraft, Aircraft Engineering and Aerospace Technology, Vol. 74, No. 6, 2002, pp. 534-549.
- [13] Tomczyk A., Facilialed Airplane - project and preliminary in-flight experiments, Aerospace Science and Technology, Vol. 8, 2004, pp. 469-477.
- [14] Small Aircraft Transportation System Website, NASA Langley Research Center, http://sats.nasa.gov, Hampton, Virginia 2005.
Typ dokumentu
Bibliografia
Identyfikator YADDA
bwmeta1.element.baztech-article-BAT5-0033-0051