FR2353090A2 - Aircraft total energy control system - has aerodynamic and selected climb or inclination modulated with respect to deviations in velocity - Google Patents

Aircraft total energy control system - has aerodynamic and selected climb or inclination modulated with respect to deviations in velocity

Info

Publication number
FR2353090A2
FR2353090A2 FR7615929A FR7615929A FR2353090A2 FR 2353090 A2 FR2353090 A2 FR 2353090A2 FR 7615929 A FR7615929 A FR 7615929A FR 7615929 A FR7615929 A FR 7615929A FR 2353090 A2 FR2353090 A2 FR 2353090A2
Authority
FR
France
Prior art keywords
inclination
aerodynamic
control system
velocity
modulated
Prior art date
Legal status (The legal status 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 status listed.)
Granted
Application number
FR7615929A
Other languages
French (fr)
Other versions
FR2353090B2 (en
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
Societe Francaise dEquipements pour la Navigation Aerienne SFENA SA
Original Assignee
Societe Francaise dEquipements pour la Navigation Aerienne SFENA SA
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 Societe Francaise dEquipements pour la Navigation Aerienne SFENA SA filed Critical Societe Francaise dEquipements pour la Navigation Aerienne SFENA SA
Priority to FR7615929A priority Critical patent/FR2353090A2/en
Priority to GB26757/76A priority patent/GB1553407A/en
Priority to CA256,222A priority patent/CA1088655A/en
Priority to IT24989/76A priority patent/IT1067300B/en
Priority to DE19762630651 priority patent/DE2630651A1/en
Publication of FR2353090A2 publication Critical patent/FR2353090A2/en
Application granted granted Critical
Publication of FR2353090B2 publication Critical patent/FR2353090B2/fr
Granted legal-status Critical Current

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
    • G05D1/0653—Rate of change of altitude or depth specially adapted for aircraft during a phase of take-off or landing
    • G05D1/0661—Rate of change of altitude or depth specially adapted for aircraft during a phase of take-off or landing specially adapted for take-off

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)
  • Control Of Position, Course, Altitude, Or Attitude Of Moving Bodies (AREA)

Abstract

A total energy control system for take off and control system of an aeroplane, controls the aerodynamic inclination (gamma a) to a selected value of inclination or climb (gamma d). This itself represents the total inclination or climb (gamma t) being modulated by the deviation of the velocity (V) from the required velocity (V2). A warning or display signal (delta) is passed between the aerodynamic inclination (gamma a) and the selected inclination (gamma d) by means of a notched positional beam (2) or by means of a Lectz horizon (3).
FR7615929A 1975-07-04 1976-05-26 Aircraft total energy control system - has aerodynamic and selected climb or inclination modulated with respect to deviations in velocity Granted FR2353090A2 (en)

Priority Applications (5)

Application Number Priority Date Filing Date Title
FR7615929A FR2353090A2 (en) 1976-05-26 1976-05-26 Aircraft total energy control system - has aerodynamic and selected climb or inclination modulated with respect to deviations in velocity
GB26757/76A GB1553407A (en) 1975-07-04 1976-06-28 Flying method and system using total energy for an aircraft
CA256,222A CA1088655A (en) 1975-07-04 1976-07-02 Flying method and system using total power for an aircraft
IT24989/76A IT1067300B (en) 1975-07-04 1976-07-02 PROCESS AND PILOTING SYSTEM USING TOTAL ENERGY
DE19762630651 DE2630651A1 (en) 1975-07-04 1976-07-05 TOTAL ENERGY CONTROL SYSTEM FOR AIRCRAFT

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
FR7615929A FR2353090A2 (en) 1976-05-26 1976-05-26 Aircraft total energy control system - has aerodynamic and selected climb or inclination modulated with respect to deviations in velocity

Publications (2)

Publication Number Publication Date
FR2353090A2 true FR2353090A2 (en) 1977-12-23
FR2353090B2 FR2353090B2 (en) 1980-05-30

Family

ID=9173664

Family Applications (1)

Application Number Title Priority Date Filing Date
FR7615929A Granted FR2353090A2 (en) 1975-07-04 1976-05-26 Aircraft total energy control system - has aerodynamic and selected climb or inclination modulated with respect to deviations in velocity

Country Status (1)

Country Link
FR (1) FR2353090A2 (en)

Also Published As

Publication number Publication date
FR2353090B2 (en) 1980-05-30

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