GB8819093D0 - Aircraft precision approach control system - Google Patents

Aircraft precision approach control system

Info

Publication number
GB8819093D0
GB8819093D0 GB888819093A GB8819093A GB8819093D0 GB 8819093 D0 GB8819093 D0 GB 8819093D0 GB 888819093 A GB888819093 A GB 888819093A GB 8819093 A GB8819093 A GB 8819093A GB 8819093 D0 GB8819093 D0 GB 8819093D0
Authority
GB
United Kingdom
Prior art keywords
control system
approach control
precision approach
aircraft precision
aircraft
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
GB888819093A
Other versions
GB2208631B (en
GB2208631A (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.)
Grumman Corp
Original Assignee
Grumman Aerospace Corp
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 Grumman Aerospace Corp filed Critical Grumman Aerospace Corp
Publication of GB8819093D0 publication Critical patent/GB8819093D0/en
Publication of GB2208631A publication Critical patent/GB2208631A/en
Application granted granted Critical
Publication of GB2208631B publication Critical patent/GB2208631B/en
Anticipated expiration legal-status Critical
Expired - Fee Related 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 or altitude of land, water, air, or space vehicles, e.g. automatic pilot
    • 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
    • G05D1/0676—Rate of change of altitude or depth specially adapted for aircraft during a phase of take-off or landing specially adapted for landing
    • G05D1/0684—Rate of change of altitude or depth specially adapted for aircraft during a phase of take-off or landing specially adapted for landing on a moving platform, e.g. aircraft carrier
GB8819093A 1987-08-13 1988-08-11 Aircraft precision approach control system Expired - Fee Related GB2208631B (en)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
US8546187A 1987-08-13 1987-08-13

Publications (3)

Publication Number Publication Date
GB8819093D0 true GB8819093D0 (en) 1988-09-14
GB2208631A GB2208631A (en) 1989-04-12
GB2208631B GB2208631B (en) 1991-06-26

Family

ID=22191768

Family Applications (1)

Application Number Title Priority Date Filing Date
GB8819093A Expired - Fee Related GB2208631B (en) 1987-08-13 1988-08-11 Aircraft precision approach control system

Country Status (6)

Country Link
JP (1) JPH01119500A (en)
CA (1) CA1317008C (en)
DE (1) DE3827482A1 (en)
FR (1) FR2619458A1 (en)
GB (1) GB2208631B (en)
IL (1) IL87382A (en)

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN117452974A (en) * 2023-12-22 2024-01-26 中国航空工业集团公司西安飞机设计研究所 Method and device for optimizing short-distance landing of conveyor airport

Families Citing this family (6)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE3621052A1 (en) * 1986-06-24 1988-01-07 Aerodata Flugmesstechnik Gmbh Device for the automatic flight path guidance of aircraft along a guidance beam
DE4300761A1 (en) * 1993-01-14 1994-07-21 Erno Raumfahrttechnik Gmbh Control device
US7609204B2 (en) 2005-08-30 2009-10-27 Honeywell International Inc. System and method for dynamically estimating output variances for carrier-smoothing filters
FR2909462B1 (en) * 2006-12-05 2008-12-26 Airbus France Sas METHOD AND DEVICE FOR ACTIVE CONTROL OF THE TANGULATION OF AN AIRCRAFT.
EP2151730A1 (en) * 2008-08-05 2010-02-10 The Boeing Company Four-dimensional navigation of an aircraft
CN104536462A (en) * 2015-01-09 2015-04-22 西安应用光学研究所 Position control method based on fiber-optic gyroscope integral means

Family Cites Families (7)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3586268A (en) * 1969-04-04 1971-06-22 William W Melvin Instrument flight system
US3626163A (en) * 1970-01-28 1971-12-07 Us Army Automatic landing system
US3743221A (en) * 1970-04-09 1973-07-03 Lear Siegler Inc Aircraft flight control apparatus
US3714825A (en) * 1970-12-29 1973-02-06 W Melvin Instrument flight system
US4040005A (en) * 1974-12-23 1977-08-02 Melvin William W Composite situation analyzer and instrument flight system
FR2559123B1 (en) * 1984-02-03 1988-11-10 Hirsch Rene METHOD AND DEVICE FOR COMPENSATING GUSTS TO AN AIRCRAFT IN FLIGHT
US4709336A (en) * 1985-01-09 1987-11-24 Sperry Corporation Descent flight path control for aircraft

Cited By (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN117452974A (en) * 2023-12-22 2024-01-26 中国航空工业集团公司西安飞机设计研究所 Method and device for optimizing short-distance landing of conveyor airport
CN117452974B (en) * 2023-12-22 2024-04-09 中国航空工业集团公司西安飞机设计研究所 Method and device for optimizing short-distance landing of conveyor airport

Also Published As

Publication number Publication date
GB2208631B (en) 1991-06-26
DE3827482A1 (en) 1989-04-06
JPH01119500A (en) 1989-05-11
IL87382A (en) 1994-07-31
CA1317008C (en) 1993-04-27
GB2208631A (en) 1989-04-12
FR2619458A1 (en) 1989-02-17

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Legal Events

Date Code Title Description
PCNP Patent ceased through non-payment of renewal fee

Effective date: 19920811