IL199629A0 - Method for the autonomous guidance of an aircraft and corresponding aircraft - Google Patents

Method for the autonomous guidance of an aircraft and corresponding aircraft

Info

Publication number
IL199629A0
IL199629A0 IL199629A IL19962909A IL199629A0 IL 199629 A0 IL199629 A0 IL 199629A0 IL 199629 A IL199629 A IL 199629A IL 19962909 A IL19962909 A IL 19962909A IL 199629 A0 IL199629 A0 IL 199629A0
Authority
IL
Israel
Prior art keywords
aircraft
environment
fixed point
field
guiding
Prior art date
Application number
IL199629A
Other versions
IL199629A (en
Original Assignee
Sagem Defense Securite
Priority date (The priority date is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the date listed.)
Filing date
Publication date
Application filed by Sagem Defense Securite filed Critical Sagem Defense Securite
Publication of IL199629A0 publication Critical patent/IL199629A0/en
Publication of IL199629A publication Critical patent/IL199629A/en

Links

Classifications

    • G—PHYSICS
    • G05—CONTROLLING; REGULATING
    • G05D—SYSTEMS FOR CONTROLLING OR REGULATING NON-ELECTRIC VARIABLES
    • G05D1/00—Control of position, course, altitude or attitude of land, water, air or space vehicles, e.g. using automatic pilots
    • G05D1/04—Control of altitude or depth
    • G05D1/06—Rate of change of altitude or depth
    • G05D1/0607—Rate of change of altitude or depth specially adapted for aircraft
    • G05D1/0646—Rate of change of altitude or depth specially adapted for aircraft to follow the profile of undulating ground

Landscapes

  • Engineering & Computer Science (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Radar, Positioning & Navigation (AREA)
  • Remote Sensing (AREA)
  • Physics & Mathematics (AREA)
  • General Physics & Mathematics (AREA)
  • Automation & Control Theory (AREA)
  • Traffic Control Systems (AREA)
  • Navigation (AREA)
  • Control Of Position, Course, Altitude, Or Attitude Of Moving Bodies (AREA)

Abstract

The invention relates to a method for guiding an aircraft (1) in an environment (2), the aircraft (1) including at least one sensor (3) with an environment-observation optical field (4), the environment (2) being displayed in the field of the sensor (3) during the movement of the aircraft relative to a fixed point (5) at the centre of the field, characterised in that it comprises the step of: determining at least two magnitudes related to the display of the environment, one magnitude being located on one side of the fixed point (5) and the other being located on the other side of the fixed point (5); determining a deviation between the two magnitudes; automatically guiding the aircraft in the environment, the guiding direction depending on said deviation. The invention also relates to an aircraft for implementing said method.
IL199629A 2007-01-04 2009-06-30 Method for the autonomous guidance of an aircraft and corresponding aircraft IL199629A (en)

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
FR0752528A FR2911194B1 (en) 2007-01-04 2007-01-04 METHOD FOR AUTONOMOUS GUIDANCE OF AN AIRCRAFT AND CORRESPONDING AIRCRAFT.
PCT/EP2008/050055 WO2008081038A1 (en) 2007-01-04 2008-01-04 Method for the autonomous guidance of an aircraft and corresponding aircraft

Publications (2)

Publication Number Publication Date
IL199629A0 true IL199629A0 (en) 2010-04-15
IL199629A IL199629A (en) 2013-08-29

Family

ID=38698359

Family Applications (1)

Application Number Title Priority Date Filing Date
IL199629A IL199629A (en) 2007-01-04 2009-06-30 Method for the autonomous guidance of an aircraft and corresponding aircraft

Country Status (5)

Country Link
EP (1) EP2115542B1 (en)
AT (1) ATE548684T1 (en)
FR (1) FR2911194B1 (en)
IL (1) IL199629A (en)
WO (1) WO2008081038A1 (en)

Family Cites Families (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
GB1605386A (en) * 1974-07-26 1995-02-01 Emi Ltd Improvements relating to vehicle guidance systems
FR2731824B1 (en) * 1995-03-17 1997-05-16 Sextant Avionique COLLISION AVOIDANCE DEVICE FOR AIRCRAFT, PARTICULARLY WITH THE GROUND

Also Published As

Publication number Publication date
WO2008081038A1 (en) 2008-07-10
ATE548684T1 (en) 2012-03-15
FR2911194B1 (en) 2009-02-27
EP2115542B1 (en) 2012-03-07
EP2115542A1 (en) 2009-11-11
IL199629A (en) 2013-08-29
FR2911194A1 (en) 2008-07-11

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