• Non ci sono risultati.

Denti, Dispense di Dinamica del Volo, Department of Aerospace Engineering, University of Pisa, 2009 [14] Prof

N/A
N/A
Protected

Academic year: 2021

Condividi "Denti, Dispense di Dinamica del Volo, Department of Aerospace Engineering, University of Pisa, 2009 [14] Prof"

Copied!
2
0
0

Testo completo

(1)

130

Bibliography

[1] Alenia Aermacchi, "M346 PA Design and Functional Description", A.AEM internal doc, 2006 [2] MIL-F-8785C, Flying Qualities of Piloted Airplanes, US DoD, Notice 2, 1996

[3] Gibson J.C., Development of a Methodology for excellence in Handling Qualities Design for Fly-by-Wire Aircraft, Delft University Press, 1999

[4] MIL-STD-1797A, Flying Qualities of Piloted Airplanes, US DoD, 1987

[5] Mitchell D.G., Klyde D.H., Recommended Practices for Exposing Pilot-Induced Oscillations or Tendencies in the Development Process, USAF Developmental Test and Evaluation Summit Woodland Hills CA, November 16-18 2004

[6] Gibson J.C., Piloted Handling Qualities Design Criteria for High Order Flight Control Systems, AGARD CP333, April 1982

[7] Gibson J.C., The Definition, Understanding and Design of Aircraft Handling Qualities, TU Delft Report LR-756,, April 1995

[8] MIL-F-9490D, Flight Control System Design, Installation and Test of Piloted Aicraft, US DoD, 1975

[9] Alenia Aermacchi, CL Design & Clearance Criteria, A.AEM internal doc, 2003

[10] Zhang Y., Jiang J., Bibliographical review on reconfigurable fault-tolerant control system, Elselvier, 2008

[11] Ying P., Yiping L.P.Y., The application of function reconfiguration for digital fly-by-wire flight control system, IEEE, 1998

[12] Zhang Y., Rabbath C.A., SU C.Y., Reconfigurable control allocation applied to an aircraft benchmark model, American Control Conference, Washington, June11-13 2008

(2)

131

[13] Prof. Eng. E. Denti, Dispense di Dinamica del Volo, Department of Aerospace Engineering, University of Pisa, 2009

[14] Prof. Eng. E. Denti, Eng. F Schettini, Esercitazioni di Dinamica del Volo, Department of Aerospace Engineering, University of Pisa, 2009

[15] Casarosa C., Meccanica del Volo, Edizione Plus, 2007, Part VII, Chapter 8

Riferimenti

Documenti correlati

The features used for the attack and the defense model is only obtained by RSS channel model that use A+S, because the defense models that used RSS channel model with A+S+F are

• Dijkstra’s algorithm for the global navigation, that is used for compute the path from the current position and the local goal.. The local goal is selected using a greedy

• Length of segment between 15 and 60 seconds, normally used 30-second intervals As last point, we observe the power spectrum of the neural signals in these segments and we

It is recent news that the “New Guidelines for internal architectures in schools” (Italian Ministerial Decree April 11 th 2013) have been approved, whose inspiration is drawn from

In this thesis, we have surveyed and demonstrated the classical and conventional methods of vehicle positioning Global Positioning System on the Autonomous Land Vehicles(ALV) and

The vertical magnetic rotor, which are analysed, has five different possible configurations based on the number of hubs and the number of permanent magnets mounted on the shaft..

A first analysis develops a building typology study of football stadiums in general analyzing in depth for : historical mentions, architectural structure and

von Doenhoff, “Theory of Wing Sections, Including a Summary of Airfoil Data”, Dover, New York, 1959.. “Materiale didattico integrativo al corso di costruzioni aeronautiche”,