GB1553407A - Flying method and system using total energy for an aircraft - Google Patents

Flying method and system using total energy for an aircraft

Info

Publication number
GB1553407A
GB1553407A GB26757/76A GB2675776A GB1553407A GB 1553407 A GB1553407 A GB 1553407A GB 26757/76 A GB26757/76 A GB 26757/76A GB 2675776 A GB2675776 A GB 2675776A GB 1553407 A GB1553407 A GB 1553407A
Authority
GB
United Kingdom
Prior art keywords
aircraft
total energy
flying method
flying
total
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.)
Expired
Application number
GB26757/76A
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
Priority claimed from FR7521137A external-priority patent/FR2316647A1/en
Priority claimed from FR7537862A external-priority patent/FR2334993A2/en
Priority claimed from FR7615929A external-priority patent/FR2353090A2/en
Application filed by Societe Francaise dEquipements pour la Navigation Aerienne SFENA SA filed Critical Societe Francaise dEquipements pour la Navigation Aerienne SFENA SA
Publication of GB1553407A publication Critical patent/GB1553407A/en
Expired 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
    • 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
    • G05D1/0055—Control of position, course, altitude or attitude of land, water, air or space vehicles, e.g. using automatic pilots with safety arrangements
    • G05D1/0077—Control of position, course, altitude or attitude of land, water, air or space vehicles, e.g. using automatic pilots with safety arrangements using redundant signals or controls

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)
GB26757/76A 1975-07-04 1976-06-28 Flying method and system using total energy for an aircraft Expired GB1553407A (en)

Applications Claiming Priority (3)

Application Number Priority Date Filing Date Title
FR7521137A FR2316647A1 (en) 1975-07-04 1975-07-04 Aircraft total energy control system - has aerodynamic and selected climb or inclination modulated with respect to deviations in velocity
FR7537862A FR2334993A2 (en) 1975-12-10 1975-12-10 Aircraft total energy control system - has aerodynamic and selected climb or inclination modulated with respect to deviations in velocity
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 (1)

Publication Number Publication Date
GB1553407A true GB1553407A (en) 1979-09-26

Family

ID=27250494

Family Applications (1)

Application Number Title Priority Date Filing Date
GB26757/76A Expired GB1553407A (en) 1975-07-04 1976-06-28 Flying method and system using total energy for an aircraft

Country Status (4)

Country Link
CA (1) CA1088655A (en)
DE (1) DE2630651A1 (en)
GB (1) GB1553407A (en)
IT (1) IT1067300B (en)

Cited By (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
EP3528080A1 (en) * 2018-02-20 2019-08-21 The Boeing Company Optimizing climb performance during takeoff using variable initial pitch angle target
CN112947520A (en) * 2021-02-08 2021-06-11 北京电子工程总体研究所 Attitude control method and device for improving stability of low-speed aircraft under stall

Families Citing this family (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US4609987A (en) * 1983-03-09 1986-09-02 Safe Flight Instrument Corporation Aircraft guidance system for take off or go-around during severe wind shear

Family Cites Families (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
GB1102781A (en) * 1965-01-20 1968-02-07 Smiths Industries Ltd Improvements in or relating to aircraft instruments
US3748980A (en) * 1971-12-06 1973-07-31 Polaroid Corp Flash socket assembly

Cited By (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
EP3528080A1 (en) * 2018-02-20 2019-08-21 The Boeing Company Optimizing climb performance during takeoff using variable initial pitch angle target
CN110174840A (en) * 2018-02-20 2019-08-27 波音公司 Climbing performance during being taken off using variable initial pitch angle objective optimization
CN110174840B (en) * 2018-02-20 2023-03-31 波音公司 Optimizing climb performance during takeoff with variable initial pitch target
CN112947520A (en) * 2021-02-08 2021-06-11 北京电子工程总体研究所 Attitude control method and device for improving stability of low-speed aircraft under stall

Also Published As

Publication number Publication date
CA1088655A (en) 1980-10-28
IT1067300B (en) 1985-03-16
DE2630651A1 (en) 1977-01-20

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Legal Events

Date Code Title Description
PS Patent sealed [section 19, patents act 1949]
PCNP Patent ceased through non-payment of renewal fee

Effective date: 19950628