JPS5643919B2 - - Google Patents

Info

Publication number
JPS5643919B2
JPS5643919B2 JP1641173A JP1641173A JPS5643919B2 JP S5643919 B2 JPS5643919 B2 JP S5643919B2 JP 1641173 A JP1641173 A JP 1641173A JP 1641173 A JP1641173 A JP 1641173A JP S5643919 B2 JPS5643919 B2 JP S5643919B2
Authority
JP
Japan
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
JP1641173A
Other languages
Japanese (ja)
Other versions
JPS4898600A (https=
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 filed Critical
Publication of JPS4898600A publication Critical patent/JPS4898600A/ja
Publication of JPS5643919B2 publication Critical patent/JPS5643919B2/ja
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
    • G05D1/08—Control of attitude, i.e. control of roll, pitch, or yaw
    • G05D1/0808—Control of attitude, i.e. control of roll, pitch, or yaw specially adapted for aircraft
    • G05D1/0858—Control of attitude, i.e. control of roll, pitch, or yaw specially adapted for aircraft specially adapted for vertical take-off of aircraft
    • 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
    • G05D1/0676—Rate of change of altitude or depth specially adapted for aircraft during a phase of take-off or landing specially adapted for landing

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)
  • Traffic Control Systems (AREA)
  • Toys (AREA)
  • Navigation (AREA)
JP1641173A 1972-02-28 1973-02-09 Expired JPS5643919B2 (https=)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
US229928A US3916688A (en) 1972-02-28 1972-02-28 VTOL craft deceleration control system

Publications (2)

Publication Number Publication Date
JPS4898600A JPS4898600A (https=) 1973-12-14
JPS5643919B2 true JPS5643919B2 (https=) 1981-10-15

Family

ID=22863254

Family Applications (1)

Application Number Title Priority Date Filing Date
JP1641173A Expired JPS5643919B2 (https=) 1972-02-28 1973-02-09

Country Status (8)

Country Link
US (1) US3916688A (https=)
JP (1) JPS5643919B2 (https=)
CA (1) CA1004331A (https=)
DE (1) DE2310045C2 (https=)
FR (1) FR2174070B1 (https=)
GB (1) GB1405236A (https=)
IT (1) IT977444B (https=)
SE (1) SE378006B (https=)

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JPS5875905A (ja) * 1981-10-30 1983-05-07 Yokogawa Hewlett Packard Ltd 増幅器

Families Citing this family (37)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US4029271A (en) * 1976-04-07 1977-06-14 United Technologies Corporation Automatic approach to hover system
FR2446469A1 (fr) * 1979-01-09 1980-08-08 Sfena Procede et dispositif de pilotage d'un aerodyne
US4413320A (en) * 1980-08-22 1983-11-01 The Bendix Corporation Control system
US4740899A (en) * 1982-07-01 1988-04-26 Rockwell International Corporation Use of headwind and airspeed to achieve a transition to a hover in a helicopter or vtol aircraft
US4551804A (en) * 1983-02-08 1985-11-05 Sperry Corporation Approach to hover control system for helicopters
US4603389A (en) * 1983-02-16 1986-07-29 Sperry Corporation Three cue flight director system for helicopters
US4980684A (en) * 1983-06-10 1990-12-25 Sundstrand Data Controls, Inc. Warning system for tactical rotary wing aircraft
US5220322A (en) * 1984-07-18 1993-06-15 Sundstrand Corporation Ground proximity warning system for use with aircraft having egraded performance
US4750127A (en) * 1985-10-31 1988-06-07 The Boeing Company Energy compensated target speed for aircraft descent
US4956780A (en) * 1988-12-08 1990-09-11 The Boeing Company Flight path angle command flight control system for landing flare
US5195039A (en) * 1990-05-03 1993-03-16 United Technologies Corporation Hover position hold system for rotary winged aircraft
US6434470B1 (en) 2000-12-05 2002-08-13 Lear Corporation Tire pressure vehicle speed limiting
US6671609B2 (en) 2000-12-05 2003-12-30 Lear Corporation Tire pressure vehicle speed limiting
US6693522B2 (en) 2001-10-12 2004-02-17 Lear Corporation System and method for tire pressure monitoring including automatic tire location recognition
US6864803B2 (en) 2001-10-12 2005-03-08 Lear Corporation System and method for tire pressure monitoring using CDMA tire pressure signals
US7154414B2 (en) * 2002-03-01 2006-12-26 Lear Corporation System and method for remote tire pressure monitoring
US6691567B2 (en) 2002-03-01 2004-02-17 Lear Corporation System and method for tire pressure monitoring including automatic tire location recognition
US6788193B2 (en) 2002-03-01 2004-09-07 Lear Corporation System and method for tire pressure monitoring providing automatic tire location recognition
US6876265B2 (en) * 2002-03-01 2005-04-05 Lear Corporation System and method for using a saw based RF transmitter for AM modulated transmission in a TPM
US6933898B2 (en) * 2002-03-01 2005-08-23 Lear Corporation Antenna for tire pressure monitoring wheel electronic device
US6668636B2 (en) 2002-03-01 2003-12-30 Lear Corporation System and method for tire pressure monitoring including tire location recognition
US20030164759A1 (en) * 2002-03-01 2003-09-04 Lear Corporation System and method for tire pressure monitoring with optimal tire pressure indication during tire pressure adjustment
US6725712B1 (en) 2002-03-01 2004-04-27 Lear Corporation System and method for tire pressure monitoring with automatic tire location recognition
US6829924B2 (en) * 2002-03-01 2004-12-14 Lear Corporation Tire pressure monitoring system with low frequency initiation approach
US6647773B2 (en) 2002-03-01 2003-11-18 Lear Corporation System and method for integrated tire pressure monitoring and passive entry
US20030164034A1 (en) * 2002-03-01 2003-09-04 Lear Corporation System and method for using a saw based RF transmitter for FM transmission in a TPM
US6838985B2 (en) * 2002-03-25 2005-01-04 Lear Corporation System and method for remote tire pressure monitoring with low frequency initiation
US20030179086A1 (en) * 2002-03-25 2003-09-25 Lear Corporation System for remote tire pressure monitoring with low frequency initiation antenna
US7699260B2 (en) * 2005-01-14 2010-04-20 Hughey Electricopter Corporation Vertical takeoff and landing aircraft using a redundant array of independent rotors
US7389163B1 (en) * 2005-02-17 2008-06-17 The Boeing Company Procedure to minimize the risk of air collision for personal mid-air vehicles
IL204509A (en) * 2010-03-15 2015-01-29 Israel Aerospace Ind Ltd Vtol aircraft landing system
FR2964573B1 (fr) * 2010-09-15 2012-09-28 Parrot Procede de pilotage d'un drone a voilure tournante a rotors multiples
IL217501A (en) 2012-01-12 2017-09-28 Israel Aerospace Ind Ltd A method and system for maneuvering aircraft
US9108741B2 (en) 2013-09-09 2015-08-18 Honeywell International Inc. Helicopter system and method for integrating collective flight director cues
US10112722B2 (en) 2015-01-15 2018-10-30 Unison Industries Llc Power control for propeller-driven aircraft
CN111103890B (zh) * 2019-12-17 2022-11-11 西北工业大学 一种高精度强鲁棒的进场着陆引导控制方法
US11358733B2 (en) 2020-01-21 2022-06-14 Rockwell Collins, Inc. Optimum idle descent start point display based on current conditions

Family Cites Families (10)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2845623A (en) * 1956-01-03 1958-07-29 Sperry Rand Corp Aircraft navigation system
GB864904A (en) * 1958-05-30 1961-04-12 Gen Electric Improvements in aircraft jet propulsion engine controls
US3096503A (en) * 1960-01-25 1963-07-02 Sperry Rand Corp Aircraft navigation system
US3265333A (en) * 1964-02-03 1966-08-09 North American Aviation Inc Override control means for automatic landing system
US3307191A (en) * 1964-03-12 1967-02-28 Carl J Crane Aircraft blind landing device and flight director system
US3333795A (en) * 1966-01-10 1967-08-01 Collins Radio Co Flare computer
US3577195A (en) * 1969-04-14 1971-05-04 Sperry Rand Corp Servoed meter apparatus
US3620488A (en) * 1969-05-29 1971-11-16 Rita A Miller Aircraft command mixing device
US3743221A (en) * 1970-04-09 1973-07-03 Lear Siegler Inc Aircraft flight control apparatus
US3652835A (en) * 1970-05-14 1972-03-28 Sperry Rand Corp Aircraft glide slope coupler system

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JPS5875905A (ja) * 1981-10-30 1983-05-07 Yokogawa Hewlett Packard Ltd 増幅器

Also Published As

Publication number Publication date
CA1004331A (en) 1977-01-25
US3916688A (en) 1975-11-04
JPS4898600A (https=) 1973-12-14
IT977444B (it) 1974-09-10
FR2174070B1 (https=) 1977-02-04
DE2310045C2 (de) 1985-07-04
FR2174070A1 (https=) 1973-10-12
GB1405236A (en) 1975-09-10
SE378006B (https=) 1975-08-11
DE2310045A1 (de) 1973-09-06

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