FR2353090A2 - Procede et systeme de pilotage utilisant l'energie totale - Google Patents

Procede et systeme de pilotage utilisant l'energie totale

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
English (en)
Other versions
FR2353090B2 (fr
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/fr
Priority to GB26757/76A priority patent/GB1553407A/en
Priority to CA256,222A priority patent/CA1088655A/fr
Priority to IT24989/76A priority patent/IT1067300B/it
Priority to DE19762630651 priority patent/DE2630651A1/de
Publication of FR2353090A2 publication Critical patent/FR2353090A2/fr
Application granted granted Critical
Publication of FR2353090B2 publication Critical patent/FR2353090B2/fr
Granted legal-status Critical Current

Links

Classifications

    • GPHYSICS
    • G05CONTROLLING; REGULATING
    • G05DSYSTEMS FOR CONTROLLING OR REGULATING NON-ELECTRIC VARIABLES
    • G05D1/00Control of position, course, altitude or attitude of land, water, air or space vehicles, e.g. using automatic pilots
    • G05D1/04Control of altitude or depth
    • G05D1/06Rate of change of altitude or depth
    • G05D1/0607Rate of change of altitude or depth specially adapted for aircraft
    • G05D1/0653Rate of change of altitude or depth specially adapted for aircraft during a phase of take-off or landing
    • G05D1/0661Rate 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)
FR7615929A 1975-07-04 1976-05-26 Procede et systeme de pilotage utilisant l'energie totale Granted FR2353090A2 (fr)

Priority Applications (5)

Application Number Priority Date Filing Date Title
FR7615929A FR2353090A2 (fr) 1976-05-26 1976-05-26 Procede et systeme de pilotage utilisant l'energie totale
GB26757/76A GB1553407A (en) 1975-07-04 1976-06-28 Flying method and system using total energy for an aircraft
CA256,222A CA1088655A (fr) 1975-07-04 1976-07-02 Methode de vol et systeme a energie totale pour avion
IT24989/76A IT1067300B (it) 1975-07-04 1976-07-02 Processo e sistema di pilotaggio utilizzanti l'energia totale
DE19762630651 DE2630651A1 (de) 1975-07-04 1976-07-05 Total-energie-steuerungssystem fuer flugzeuge

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
FR7615929A FR2353090A2 (fr) 1976-05-26 1976-05-26 Procede et systeme de pilotage utilisant l'energie totale

Publications (2)

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

Family

ID=9173664

Family Applications (1)

Application Number Title Priority Date Filing Date
FR7615929A Granted FR2353090A2 (fr) 1975-07-04 1976-05-26 Procede et systeme de pilotage utilisant l'energie totale

Country Status (1)

Country Link
FR (1) FR2353090A2 (fr)

Also Published As

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

Similar Documents

Publication Publication Date Title
GB1524263A (en) Area navigation systems for aircraft
GB1523887A (en) Aircraft take-off and landing system and method for using same
GB1316485A (en) Landing control system for aircraft
GB1520173A (en) Method of controlling the flight path of a lowflying aircraft
GB1131732A (en) Improvements in and relating to automatic control systems for aircraft
FR2316647A1 (fr) Procede et systeme de pilotage utilisant l'energie totale
US4442490A (en) Aircraft pitch stabilization apparatus
GB964595A (en) Aircraft landing system
ES8707458A1 (es) Disposicion para la ejecucion de funciones relacionadas con los pasajeros yno acompanante de vuelo en un avion
GB1178673A (en) Improvements in and relating to the Control of Aircraft
GB942392A (en) Aircraft flight control systems
FR2334993A2 (fr) Procede et systeme de pilotage utilisant l'energie totale
GB1060969A (en) Airplane instrument for furnishing an indicator signal to indicate the necessity for or to control corrective action for offsetting decrease in head wind during landing approach
GB1395448A (en) Aircraft control system
GB1340448A (en) Aircraft ground speed control system
GB962117A (en) Servo-operated control systems for dirigible craft
GB1141453A (en) Aircraft landing systems
FR2322400A1 (fr) Dispositif d'elimination de la nutation residuelle d'un spationef
JPS5393533A (en) System for controlling unmanned travelling vehicles
Grgurich et al. STOLAND[Final Report]
GB1375181A (fr)
FR2434081A1 (fr) Indicateur de pente d'atterrissage pour aeronefs
GB1415692A (en) Aircraft instruments
GB952333A (en) Improvements in and relating to the linking of twin-component aviation systems
GREWAL On the Riccati controlled terminal landing of unpowered lifting vehicles(Riccati controlled feedback for guiding spacecraft during unpowered terminal phase of flight)[Ph. D. Thesis]