Skip to main content
Top

2017 | OriginalPaper | Chapter

6. Fly-by-Wire/Light Demonstrators

Activate our intelligent search to find suitable subject content or patents.

search-config
loading …

Abstract

In the case of conventional aircraft, the pilot control commands from the control devices in the cockpit are transmitted directly to the aerodynamic control surfaces such as elevator, aileron, and rudder via mechanical connections consisting of cables and rods, or by means intermediary boosters. For very large aircraft with high control forces and large structural deformations, rotary shafts (torsion bars) are also employed.

Dont have a licence yet? Then find out more about our products and how to get one now:

Springer Professional "Wirtschaft+Technik"

Online-Abonnement

Mit Springer Professional "Wirtschaft+Technik" erhalten Sie Zugriff auf:

  • über 102.000 Bücher
  • über 537 Zeitschriften

aus folgenden Fachgebieten:

  • Automobil + Motoren
  • Bauwesen + Immobilien
  • Business IT + Informatik
  • Elektrotechnik + Elektronik
  • Energie + Nachhaltigkeit
  • Finance + Banking
  • Management + Führung
  • Marketing + Vertrieb
  • Maschinenbau + Werkstoffe
  • Versicherung + Risiko

Jetzt Wissensvorsprung sichern!

Springer Professional "Technik"

Online-Abonnement

Mit Springer Professional "Technik" erhalten Sie Zugriff auf:

  • über 67.000 Bücher
  • über 390 Zeitschriften

aus folgenden Fachgebieten:

  • Automobil + Motoren
  • Bauwesen + Immobilien
  • Business IT + Informatik
  • Elektrotechnik + Elektronik
  • Energie + Nachhaltigkeit
  • Maschinenbau + Werkstoffe




 

Jetzt Wissensvorsprung sichern!

Literature
1.
go back to reference Hamel, P.: Challenges of Flight Systems—A View from the Past to the Future. In German, Invited Paper, TUHH, 19 Apr 2010 Hamel, P.: Challenges of Flight Systems—A View from the Past to the Future. In German, Invited Paper, TUHH, 19 Apr 2010
2.
go back to reference Croft, J.: Problematic Probe—Inaccurate Airspeed Readings Due to Ice Crystals Prompted Unnecessary Dives on a United Flight, AW&ST, pp. 32–33, May 23–June 5, 2016 Croft, J.: Problematic Probe—Inaccurate Airspeed Readings Due to Ice Crystals Prompted Unnecessary Dives on a United Flight, AW&ST, pp. 32–33, May 23–June 5, 2016
4.
go back to reference Sutherland, J.P.: Fly-by-Wire Flight Control Systems, Joint Meeting of Flight Mechanics and Guidance and Control Panels of AGARD, Oslo, Norway, 3 Sept 1968 Sutherland, J.P.: Fly-by-Wire Flight Control Systems, Joint Meeting of Flight Mechanics and Guidance and Control Panels of AGARD, Oslo, Norway, 3 Sept 1968
5.
6.
go back to reference Bollay, W.: Aerodynamic stability and automatic control. Annual Wright Brothers Lecture, December (1950) Bollay, W.: Aerodynamic stability and automatic control. Annual Wright Brothers Lecture, December (1950)
7.
go back to reference Milliken, W. Jr.: Dynamic stability and control research. In: Proceedings, 3rd Anglo-American Aeronautical Conference, Brighton (1951) Milliken, W. Jr.: Dynamic stability and control research. In: Proceedings, 3rd Anglo-American Aeronautical Conference, Brighton (1951)
8.
go back to reference Schmitt, V. R., Morris, J. W., Jenney G. D.: Fly-by-Wire—A Historical and Design Perspective. SAE International (1998) Schmitt, V. R., Morris, J. W., Jenney G. D.: Fly-by-Wire—A Historical and Design Perspective. SAE International (1998)
9.
go back to reference Tomayko, J. E.: Computers take Flight: a history of NASA’s pioneering digital fly-by-wire project. NASA SP 2000–4224 (2000) Tomayko, J. E.: Computers take Flight: a history of NASA’s pioneering digital fly-by-wire project. NASA SP 2000–4224 (2000)
10.
go back to reference McRuer, D., Graham, D.: A flight control century: triumphs of the systems approach. AIAA J. Guidance Control Dyn. 27(2), 161–173 (2003)CrossRef McRuer, D., Graham, D.: A flight control century: triumphs of the systems approach. AIAA J. Guidance Control Dyn. 27(2), 161–173 (2003)CrossRef
11.
go back to reference Hamel, P.: The Birth of Sweepback—related research at LFA-Germany. AIAA J. Aircraft 42(4), 01–813 (2005) Hamel, P.: The Birth of Sweepback—related research at LFA-Germany. AIAA J. Aircraft 42(4), 01–813 (2005)
12.
go back to reference Meyer, H.U. (Hrsg.): Die Pfeilflügelentwicklung in Deutschland bis 1945, Die Deutsche Luftfahrt, Band 33, Bernard & Graefe Verlag, ISBN 3–7637-6130-6 (2006) Meyer, H.U. (Hrsg.): Die Pfeilflügelentwicklung in Deutschland bis 1945, Die Deutsche Luftfahrt, Band 33, Bernard & Graefe Verlag, ISBN 3–7637-6130-6 (2006)
13.
go back to reference White, R.J.: Investigation of lateral dynamic stability in the XB-47 airplane. J. Aeronaut. Sci. 17(3), 133–149 (1950)CrossRef White, R.J.: Investigation of lateral dynamic stability in the XB-47 airplane. J. Aeronaut. Sci. 17(3), 133–149 (1950)CrossRef
14.
go back to reference Campagna, P.: Storms of Controversy: The Secret Avro Arrow Files Revealed. Dundurn Press (2010) Campagna, P.: Storms of Controversy: The Secret Avro Arrow Files Revealed. Dundurn Press (2010)
15.
go back to reference Holloway, R. B. et al.: Introduction of CCV Technology Into Airplane Design, Aircraft Design Integration and Optimization, AGARD CP-147, Paper 24, October 1973 Holloway, R. B. et al.: Introduction of CCV Technology Into Airplane Design, Aircraft Design Integration and Optimization, AGARD CP-147, Paper 24, October 1973
16.
go back to reference Morris, A.: MDO—A tool for the future. Aerogram 9(4), 19–24 (1999) Morris, A.: MDO—A tool for the future. Aerogram 9(4), 19–24 (1999)
18.
go back to reference Tomayko, J. E.: Blind Faith: The United States Air Force and the Development of Fly-by-Wire Technology. In: Neufeld, J. et al. (ed.) Technology and the Air Force—A Retrospective Assessment, CreateSpace Independent Publishing Platform, pp. 163–185 (2012) Tomayko, J. E.: Blind Faith: The United States Air Force and the Development of Fly-by-Wire Technology. In: Neufeld, J. et al. (ed.) Technology and the Air Force—A Retrospective Assessment, CreateSpace Independent Publishing Platform, pp. 163–185 (2012)
19.
go back to reference Reerink, H.P. (ed.): BGT—Die Geschichte eines Hochtechnologie-Unternehmens. Diehl BGT Defence GmbH & Co. KG, Überlingen (2006) Reerink, H.P. (ed.): BGT—Die Geschichte eines Hochtechnologie-Unternehmens. Diehl BGT Defence GmbH & Co. KG, Überlingen (2006)
20.
go back to reference Schubert H. (Ed.): Die Deutschen Senkrechtstart-Flugzeuge EWR VJ 101C, Dornier Do 31 und VFW VAK 191B – Historische Nachlese und Bewertung, DGLR-Bericht 2000–01, Bonn (2000) Schubert H. (Ed.): Die Deutschen Senkrechtstart-Flugzeuge EWR VJ 101C, Dornier Do 31 und VFW VAK 191B – Historische Nachlese und Bewertung, DGLR-Bericht 2000–01, Bonn (2000)
22.
go back to reference Matranga, G. J. et al.: Unconventional, Contrary, and Ugly: The Lunar Landing Research Vehicle. NASA SP-2004-4535 (2005) Matranga, G. J. et al.: Unconventional, Contrary, and Ugly: The Lunar Landing Research Vehicle. NASA SP-2004-4535 (2005)
24.
go back to reference Smyth, R.: Vertikal startendes und landendes Aufklärungs- und Kampfflugzeug VAK191B Technologie-Träger, DGLR-Vortrag, Hamburg, 22 June 2007 Smyth, R.: Vertikal startendes und landendes Aufklärungs- und Kampfflugzeug VAK191B Technologie-Träger, DGLR-Vortrag, Hamburg, 22 June 2007
25.
go back to reference Morgan, M.: Keeping the pilot happy—the contribution of research and development. Aeronaut. J. 75, 630–647 (1971) Morgan, M.: Keeping the pilot happy—the contribution of research and development. Aeronaut. J. 75, 630–647 (1971)
26.
go back to reference Hunt, G.H.: The evolution of fly-by-wire control techniques in the UK. Aeronaut. J. 83(821), 165–174 (1979) Hunt, G.H.: The evolution of fly-by-wire control techniques in the UK. Aeronaut. J. 83(821), 165–174 (1979)
27.
go back to reference Anon.: RAE Electric Hunter, FLIGHT International, pp. 1010–1011, June 28, 1973 Anon.: RAE Electric Hunter, FLIGHT International, pp. 1010–1011, June 28, 1973
28.
go back to reference Warwick, G.: Fly-by-Wire Jaguar, FLIGHT International, p. 816, 12 Sept 1981 Warwick, G.: Fly-by-Wire Jaguar, FLIGHT International, p. 816, 12 Sept 1981
29.
go back to reference Moxon, J.: One-Eleven Trail Blazers, Flight International, pp. 32–36. 7 Sept 1985 Moxon, J.: One-Eleven Trail Blazers, Flight International, pp. 32–36. 7 Sept 1985
30.
go back to reference Mcloughlin, A.: Smart fly by light, lucas aerospace flight control systems. Presentations at the Institution of Electrical Engineers (IEE) and British Computer Society (1994) Mcloughlin, A.: Smart fly by light, lucas aerospace flight control systems. Presentations at the Institution of Electrical Engineers (IEE) and British Computer Society (1994)
31.
go back to reference Landis K. H. et al.: Advanced flight control technology achievements at Boeing helicopters. In: Tischler M. B. (ed.): Advances in Flight Control. CRC Press, pp. 103–141 (1996) Landis K. H. et al.: Advanced flight control technology achievements at Boeing helicopters. In: Tischler M. B. (ed.): Advances in Flight Control. CRC Press, pp. 103–141 (1996)
32.
go back to reference Picirillo, A. C.: Fly-by-Wire: making the electric jet. In: NASA’s Contributions to Aeronautics. NASA SP 2010-570 1, 631–733 (2010) Picirillo, A. C.: Fly-by-Wire: making the electric jet. In: NASA’s Contributions to Aeronautics. NASA SP 2010-570 1, 631–733 (2010)
33.
go back to reference Landis, K.H., et al.: Advanced flight control technology achievements at Boeing helicopters. Int. J. Control 59(1), 263–290 (1994)CrossRef Landis, K.H., et al.: Advanced flight control technology achievements at Boeing helicopters. Int. J. Control 59(1), 263–290 (1994)CrossRef
34.
go back to reference Terry, J. L. et al.: The Advanced Digital-Optical Control System (ADOCS) User Demonstration Program, USAAVSCOM TM-89-D-2, September 1989 Terry, J. L. et al.: The Advanced Digital-Optical Control System (ADOCS) User Demonstration Program, USAAVSCOM TM-89-D-2, September 1989
35.
go back to reference Norton, W. J.: Advanced Electromechanical Actuation System (EMAS) Flight Test, 4950th Test Wing FTR-86-4, June 1986 Norton, W. J.: Advanced Electromechanical Actuation System (EMAS) Flight Test, 4950th Test Wing FTR-86-4, June 1986
36.
go back to reference Linch, N.: Dream Machine—Thrust Vectoring in the F-16, AcesAero.com (1995) Linch, N.: Dream Machine—Thrust Vectoring in the F-16, AcesAero.com (1995)
37.
go back to reference Jensen, S. C., Jenney G. D., Raymond, B., Dawson, D.: Flight test experience with an electromechanical actuator on the F-18 systems research aircraft. NASA TM-2000-209015 (2000) Jensen, S. C., Jenney G. D., Raymond, B., Dawson, D.: Flight test experience with an electromechanical actuator on the F-18 systems research aircraft. NASA TM-2000-209015 (2000)
38.
go back to reference Boris, S.: Flying Testbeds and In-Flight Simulators—An Efficient Instrument for Joint Research within European Projects. EU-Russia Aeronautics Research Cooperation Workshop, Moscow, Russia, 20–21 Oct 2003 Boris, S.: Flying Testbeds and In-Flight Simulators—An Efficient Instrument for Joint Research within European Projects. EU-Russia Aeronautics Research Cooperation Workshop, Moscow, Russia, 20–21 Oct 2003
39.
go back to reference Belyakov, R.A., Marmain, J.: MiG—Fifty Years of Secret Aircraft Design. Naval Institute Press, Annapolis, Maryland (1994) Belyakov, R.A., Marmain, J.: MiG—Fifty Years of Secret Aircraft Design. Naval Institute Press, Annapolis, Maryland (1994)
40.
go back to reference Gordon, Y., Gunston, B.: Soviet X-Planes. Midland Publishing (2000) Gordon, Y., Gunston, B.: Soviet X-Planes. Midland Publishing (2000)
41.
go back to reference Gordon, Y., Komissarov, D.: Soviet and Russian Testbed Aircraft. Hikoki Publication Ltd. (2011) Gordon, Y., Komissarov, D.: Soviet and Russian Testbed Aircraft. Hikoki Publication Ltd. (2011)
42.
go back to reference Chatrenet, D.: Use of ground-based simulators and in-flight simulation for the development of the A320 flight control system. In: Flight Research at Ames—Fifty Years of Development and Validation of Aeronautical Technology, NASA SP-1998-3300, Paper 19 (1991) Chatrenet, D.: Use of ground-based simulators and in-flight simulation for the development of the A320 flight control system. In: Flight Research at Ames—Fifty Years of Development and Validation of Aeronautical Technology, NASA SP-1998-3300, Paper 19 (1991)
43.
go back to reference Kubo, Y. et al.: The development of FBW flight control system and flight management system for ATIC BK117 experimental helicopter. In: American Helicopter Society 57th Annual Forum, Washington, DC, 9–11 May 2001 Kubo, Y. et al.: The development of FBW flight control system and flight management system for ATIC BK117 experimental helicopter. In: American Helicopter Society 57th Annual Forum, Washington, DC, 9–11 May 2001
44.
go back to reference Metzdorff, W.: Elektro-hydraulische Stellglieder für die digitale Steuerungs- und Regelungstechnik, VDI-Bericht Nr. 107 (1966) Metzdorff, W.: Elektro-hydraulische Stellglieder für die digitale Steuerungs- und Regelungstechnik, VDI-Bericht Nr. 107 (1966)
45.
go back to reference Metzdorff, W.: Neuere Arbeiten zur Flugzeug-Primärsteuerung am Institut für Flugführung der DFL, DFL-Mitteilungen, Heft 8, Seiten 393–404 (1968) Metzdorff, W.: Neuere Arbeiten zur Flugzeug-Primärsteuerung am Institut für Flugführung der DFL, DFL-Mitteilungen, Heft 8, Seiten 393–404 (1968)
46.
go back to reference Metzdorff, W.: Zuverlässigkeit digitaler elektronischer Flugzeug-Primärsteuersysteme, DLR-FB 73–85 (1973) Metzdorff, W.: Zuverlässigkeit digitaler elektronischer Flugzeug-Primärsteuersysteme, DLR-FB 73–85 (1973)
47.
go back to reference Hobson, Engineering Proposal: Triplex Electro-hydraulic Actuator. Report No. ED/357/2/EP-1, 25. Wolverhampton, September (1964) Hobson, Engineering Proposal: Triplex Electro-hydraulic Actuator. Report No. ED/357/2/EP-1, 25. Wolverhampton, September (1964)
48.
go back to reference Tersteegen, J.: Einbau einer digitalen elektrohydraulischen Flugzeug-Primärsteuerung in das Forschungsschiff “Planet” zur Langzeit-erprobung, DFVLR-IB 082-72/15, April 1972 Tersteegen, J.: Einbau einer digitalen elektrohydraulischen Flugzeug-Primärsteuerung in das Forschungsschiff “Planet” zur Langzeit-erprobung, DFVLR-IB 082-72/15, April 1972
49.
go back to reference Hartmann, U.: Übertragungsverhalten des STOL-Flugzeuges Do 28D Skyservant, BGT TB 000D350/68 (1968) Hartmann, U.: Übertragungsverhalten des STOL-Flugzeuges Do 28D Skyservant, BGT TB 000D350/68 (1968)
50.
go back to reference Böhret, H., Schänzer, G.: The influence of microwave landing systems on guidance and control. In: AGARD Guidance and Control Panel Symposium on Night and All Weather Guidance and Control Systems for Fixed-Wing Aircraft, Cheltenham Spa, 3–6 May 1976 Böhret, H., Schänzer, G.: The influence of microwave landing systems on guidance and control. In: AGARD Guidance and Control Panel Symposium on Night and All Weather Guidance and Control Systems for Fixed-Wing Aircraft, Cheltenham Spa, 3–6 May 1976
51.
go back to reference Schänzer, G.: Auslegung von Autopiloten durch Zustandsrückführung, Regelungstechnik, 26. Jahrgang, Heft 3, Seiten 75–104 (1978) Schänzer, G.: Auslegung von Autopiloten durch Zustandsrückführung, Regelungstechnik, 26. Jahrgang, Heft 3, Seiten 75–104 (1978)
52.
go back to reference Schänzer, G.: Direct Lift Control for Flight Control and Gust Alleviation. AGARD Guidance and Control Panel Symposium on Guidance and Control Design Considerations for Low Altitudes and Terminal Flight, Dayton, Ohio, October 1977 Schänzer, G.: Direct Lift Control for Flight Control and Gust Alleviation. AGARD Guidance and Control Panel Symposium on Guidance and Control Design Considerations for Low Altitudes and Terminal Flight, Dayton, Ohio, October 1977
53.
go back to reference Krag, B., Subke, H.: Flugversuche im Windkanal zur Entwicklung und Erprobung eines Böenenabminderungssystems. DFVLR Nachrichten, Heft 7, Seiten 561–562, Juli 1974 Krag, B., Subke, H.: Flugversuche im Windkanal zur Entwicklung und Erprobung eines Böenenabminderungssystems. DFVLR Nachrichten, Heft 7, Seiten 561–562, Juli 1974
54.
go back to reference Chambers, J.: Modeling flight—the role of dynamically scaled free-flight models in support of NASA’s aerospace programs. NASA SP 2009–575 (2010) Chambers, J.: Modeling flight—the role of dynamically scaled free-flight models in support of NASA’s aerospace programs. NASA SP 2009–575 (2010)
55.
go back to reference Heumann, G. W.: Das AVS-Projekt. Deutsch-amerikanisches Mehrzweck-VSTOL-Kampfflugzeug. FLUGREVUE 1967/4, S. 14–16 Heumann, G. W.: Das AVS-Projekt. Deutsch-amerikanisches Mehrzweck-VSTOL-Kampfflugzeug. FLUGREVUE 1967/4, S. 14–16
56.
go back to reference Krag, B., Subke, H.: Dynamic simulation in wind tunnels, part II. In: 46th Meeting Flight Mechanics Panel on Flight/Ground Testing Facilities Correlation, Valloire, June 9–13, 1975, AGARD CP 187, Paper 5 (1975) Krag, B., Subke, H.: Dynamic simulation in wind tunnels, part II. In: 46th Meeting Flight Mechanics Panel on Flight/Ground Testing Facilities Correlation, Valloire, June 9–13, 1975, AGARD CP 187, Paper 5 (1975)
57.
go back to reference Hoffmann, G.: Stabilisierung, Böenkom-pensation und Schwingungsdämpfung am elastischen, beweglichen Flugzeugmodell im Windkanal. Deutsche Luft- und Raumfahrt, DLR-FB 76–44 (1976) Hoffmann, G.: Stabilisierung, Böenkom-pensation und Schwingungsdämpfung am elastischen, beweglichen Flugzeugmodell im Windkanal. Deutsche Luft- und Raumfahrt, DLR-FB 76–44 (1976)
58.
go back to reference Krag, B., Wünnenberg, H.: OLGA, a gust alleviation system for improvement of passenger comfort of general aviation aircraft. Vortrag auf dem 12. ICAS-Congress in München, Oktober (1980) Krag, B., Wünnenberg, H.: OLGA, a gust alleviation system for improvement of passenger comfort of general aviation aircraft. Vortrag auf dem 12. ICAS-Congress in München, Oktober (1980)
59.
go back to reference Böhret, H., Krag, B., Skudridakis, J.: OLGA—open loop gust alleviation system AGARD CP 384. Paper 13 (1984) Böhret, H., Krag, B., Skudridakis, J.: OLGA—open loop gust alleviation system AGARD CP 384. Paper 13 (1984)
60.
go back to reference Löbert, G.: CCV Reglergestützte Flugzeuge, MBB-UF-Bericht, S. 84–91 Löbert, G.: CCV Reglergestützte Flugzeuge, MBB-UF-Bericht, S. 84–91
61.
go back to reference Esch, P., Wünnenberg, H.: Direct side force and drag control with the aid of pylon split flaps. AGARD CP-262, Paper 10 (1979) Esch, P., Wünnenberg, H.: Direct side force and drag control with the aid of pylon split flaps. AGARD CP-262, Paper 10 (1979)
62.
go back to reference Jacob, D., Welte, D., Wünnenberg, H.: Experimental Flight Test Programs for improving Combat Aircraft Manoeuvrability by Manoeuvre Flaps and Pylon Split Flaps, AGARD CP-319, Paper 10, October 1981 Jacob, D., Welte, D., Wünnenberg, H.: Experimental Flight Test Programs for improving Combat Aircraft Manoeuvrability by Manoeuvre Flaps and Pylon Split Flaps, AGARD CP-319, Paper 10, October 1981
63.
go back to reference Pletschacher, P.: DASA/Rockwell X-31A: Auf dem Absatz kehrt, Aerospace 1/95, S. 12-15 (1995) Pletschacher, P.: DASA/Rockwell X-31A: Auf dem Absatz kehrt, Aerospace 1/95, S. 12-15 (1995)
64.
go back to reference Beh, H., Hofinger, G.: X-31A Control Law Design. AGARD CP-548, Paper 13, March 1994 Beh, H., Hofinger, G.: X-31A Control Law Design. AGARD CP-548, Paper 13, March 1994
65.
go back to reference Hamel, P., Jategaonkar, R.: Evolution of flight vehicle system identification. AIAA J. Aircraft 33(1), 9–28 (1996) Hamel, P., Jategaonkar, R.: Evolution of flight vehicle system identification. AIAA J. Aircraft 33(1), 9–28 (1996)
66.
go back to reference Weiss, S., Friehmelt, H., Plaetschke, E. Rohlf, D.: X-31A system identification using single surface excitation at high angles of attack. AIAA Paper 95-3436, August 1995 Weiss, S., Friehmelt, H., Plaetschke, E. Rohlf, D.: X-31A system identification using single surface excitation at high angles of attack. AIAA Paper 95-3436, August 1995
67.
go back to reference Rohlf, D.: Direct Update of a Global Simulation Model with Increments via System Identification, RTO-MP-11. Paper No. 28, March 1999 Rohlf, D.: Direct Update of a Global Simulation Model with Increments via System Identification, RTO-MP-11. Paper No. 28, March 1999
68.
go back to reference Bosworth, J. T., Stoliker, P. C.: The X-31A Quasi-Tailless Flight Test Reults, NASA Technical Paper 3624 (1996) Bosworth, J. T., Stoliker, P. C.: The X-31A Quasi-Tailless Flight Test Reults, NASA Technical Paper 3624 (1996)
69.
go back to reference Rohlf, D., Brieger, O., Grohs, T.: X-31 VECTOR System Identification—Approach and Results, AIAA-2004-4830 (2004) Rohlf, D., Brieger, O., Grohs, T.: X-31 VECTOR System Identification—Approach and Results, AIAA-2004-4830 (2004)
70.
go back to reference Rohlf, D.: Global model approach for X-31 VECTOR system identification. J. Aircraft 42(1) (2005) Rohlf, D.: Global model approach for X-31 VECTOR system identification. J. Aircraft 42(1) (2005)
71.
go back to reference Huber, P.: X-31 VECTOR Technologieprogramm – Der Ritt auf dem Strahl, Hochschule für Angewandte Wissenschaften Hamburg, 13 March 2003 Huber, P.: X-31 VECTOR Technologieprogramm – Der Ritt auf dem Strahl, Hochschule für Angewandte Wissenschaften Hamburg, 13 March 2003
72.
go back to reference Ross, H., Robinson, M.: X-31: 20 Jahre erfolgreiche internationale Zusammenarbeit zwischen Deutschland und den USA, DGLR-JT2003-053 (2003) Ross, H., Robinson, M.: X-31: 20 Jahre erfolgreiche internationale Zusammenarbeit zwischen Deutschland und den USA, DGLR-JT2003-053 (2003)
73.
go back to reference Grohs, T., Fischer, B., Heinzinger, O., Brieger, O.: X-31 VECTOR—ESTOL to the ground—flight test results and lessons learned. AIAA-2004-5029, August 2004 Grohs, T., Fischer, B., Heinzinger, O., Brieger, O.: X-31 VECTOR—ESTOL to the ground—flight test results and lessons learned. AIAA-2004-5029, August 2004
74.
go back to reference Luckner, R., Dalldorff, L., Reichel R.: A utility aircraft for remote sensing missions with a high-precision automatic flight control system. IEEE international conference on aerospace electronics and remote sensing technology 2014 (ICARES), Yogyakarta, Indonesia (2014) Luckner, R., Dalldorff, L., Reichel R.: A utility aircraft for remote sensing missions with a high-precision automatic flight control system. IEEE international conference on aerospace electronics and remote sensing technology 2014 (ICARES), Yogyakarta, Indonesia (2014)
76.
go back to reference Anon.: F3061, Standard Specification for Systems and Equipment in Small Aircraft. ASTM Committee F44 on General Aviation Aircraft, current edition approved August 1, 2016. Published September 2016 Anon.: F3061, Standard Specification for Systems and Equipment in Small Aircraft. ASTM Committee F44 on General Aviation Aircraft, current edition approved August 1, 2016. Published September 2016
77.
go back to reference Goerke, S., Riebeling, R., Kraus, F., Reichel, R.: Flexible platform approach for fly-by-wire systems. IEEE/AIAA 32nd digital avionics systems conference (DASC), pp. 2C5-1–2C5-16, 25–29 Sept 2016 Goerke, S., Riebeling, R., Kraus, F., Reichel, R.: Flexible platform approach for fly-by-wire systems. IEEE/AIAA 32nd digital avionics systems conference (DASC), pp. 2C5-1–2C5-16, 25–29 Sept 2016
78.
go back to reference Mueller, P., Belschner, T., Lehmann, M., Reichel, R.: AAA-process—A New Approach to Affordable Fly-by-Wire Systems for CS23 Aircraft, DGLR Congress 2016, Braunschweig, Germany (2016) Mueller, P., Belschner, T., Lehmann, M., Reichel, R.: AAA-process—A New Approach to Affordable Fly-by-Wire Systems for CS23 Aircraft, DGLR Congress 2016, Braunschweig, Germany (2016)
Metadata
Title
Fly-by-Wire/Light Demonstrators
Author
Peter G. Hamel
Copyright Year
2017
DOI
https://doi.org/10.1007/978-3-319-53997-3_6

Premium Partner