GB1461035A - Apparatus for stabilisation of an aircraft moored by a cable - Google Patents

Apparatus for stabilisation of an aircraft moored by a cable

Info

Publication number
GB1461035A
GB1461035A GB561075A GB561075A GB1461035A GB 1461035 A GB1461035 A GB 1461035A GB 561075 A GB561075 A GB 561075A GB 561075 A GB561075 A GB 561075A GB 1461035 A GB1461035 A GB 1461035A
Authority
GB
United Kingdom
Prior art keywords
cable
gyro
tension
aircraft
signals
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
GB561075A
Other languages
English (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.)
Dornier GmbH
Original Assignee
Dornier GmbH
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 Dornier GmbH filed Critical Dornier GmbH
Publication of GB1461035A publication Critical patent/GB1461035A/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
    • G05D1/08—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
    • G05D1/0866—Control of attitude, i.e. control of roll, pitch, or yaw specially adapted for aircraft specially adapted to captive 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
    • G05D1/08—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
    • G05D1/0816—Control of attitude, i.e. control of roll, pitch, or yaw specially adapted for aircraft to ensure stability
    • G05D1/0841—Control of attitude, i.e. control of roll, pitch, or yaw specially adapted for aircraft to ensure stability to prevent a coupling between different modes

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)
GB561075A 1974-03-14 1975-02-10 Apparatus for stabilisation of an aircraft moored by a cable Expired GB1461035A (en)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
DE2412256A DE2412256C3 (de) 1974-03-14 1974-03-14 Einrichtung zur Stabilisierung von einseil-gefesselten Fluggeräten

Publications (1)

Publication Number Publication Date
GB1461035A true GB1461035A (en) 1977-01-13

Family

ID=5910062

Family Applications (1)

Application Number Title Priority Date Filing Date
GB561075A Expired GB1461035A (en) 1974-03-14 1975-02-10 Apparatus for stabilisation of an aircraft moored by a cable

Country Status (4)

Country Link
DE (1) DE2412256C3 (https=)
FR (1) FR2264318B1 (https=)
GB (1) GB1461035A (https=)
IT (1) IT1060062B (https=)

Cited By (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN109835498A (zh) * 2017-11-24 2019-06-04 天津职业技术师范大学 基于有线动力供给及数据传输的无人机系统及其实现方法
CN109911239A (zh) * 2019-04-09 2019-06-21 珠海市双捷科技有限公司 系留无人机用放线长度控制装置、绞盘装置及无人机系统

Cited By (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN109835498A (zh) * 2017-11-24 2019-06-04 天津职业技术师范大学 基于有线动力供给及数据传输的无人机系统及其实现方法
CN109911239A (zh) * 2019-04-09 2019-06-21 珠海市双捷科技有限公司 系留无人机用放线长度控制装置、绞盘装置及无人机系统
CN109911239B (zh) * 2019-04-09 2023-10-31 珠海市双捷科技有限公司 系留无人机用放线长度控制装置、绞盘装置及无人机系统

Also Published As

Publication number Publication date
FR2264318B1 (https=) 1980-07-18
DE2412256C3 (de) 1979-06-07
FR2264318A1 (https=) 1975-10-10
DE2412256A1 (de) 1975-09-18
DE2412256B2 (de) 1978-10-05
IT1060062B (it) 1982-07-10

Similar Documents

Publication Publication Date Title
US6847865B2 (en) Miniature, unmanned aircraft with onboard stabilization and automated ground control of flight path
JP4377332B2 (ja) 航空機の高度及び垂直線に対して直角方向の水平速度の操縦支援システム、及びこれを具備する航空機
WO1997020734A3 (en) Flight control system for jet powered tri-mode aircraft
EP0321876A2 (en) Control system for helicopters
US3711042A (en) Aircraft control system
GB1316485A (en) Landing control system for aircraft
CA2113731A1 (en) Automatic Turn Coordination Trim Control for Rotary Wing Aircraft
US6076024A (en) Earth-referenced wind adjustment for hovering aircraft
GB1131732A (en) Improvements in and relating to automatic control systems for aircraft
GB1181668A (en) Improvements relating to Air Responsive Apparatus
JP3292859B2 (ja) 自動操縦装置を具備した物量投下用落下傘
GB1023831A (en) Automatic trim correcting system for aircraft
GB1461035A (en) Apparatus for stabilisation of an aircraft moored by a cable
GB1053713A (https=)
US2799461A (en) Automatic air speed control
US3094299A (en) Autopilot
US4095759A (en) Device for stabilization of captive aircraft
GB1593631A (en) Means for setting down loads from transport aircraft
GB999007A (en) Improvements in or relating to automatic transition devices for v.t.o.l. aircraft
GB911082A (en) Improvements relating to control apparatus for helicopters
US3228629A (en) Rotary wing aircraft having autopiloting means
GB1182541A (en) Automatic Pilots for Aircraft
USRE26064E (en) Longitudinal mode
GB789098A (en) Improvements in or relating to stabilising and control devices for aircraft
GB1059961A (en) Improvements in and relating to helicopters with rigid rotors

Legal Events

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