SG11201405891PA - Altitude regulator - Google Patents

Altitude regulator

Info

Publication number
SG11201405891PA
SG11201405891PA SG11201405891PA SG11201405891PA SG11201405891PA SG 11201405891P A SG11201405891P A SG 11201405891PA SG 11201405891P A SG11201405891P A SG 11201405891PA SG 11201405891P A SG11201405891P A SG 11201405891PA SG 11201405891P A SG11201405891P A SG 11201405891PA
Authority
SG
Singapore
Prior art keywords
altitude regulator
altitude
regulator
Prior art date
Application number
SG11201405891PA
Inventor
Trygve Frederik Marton
Mellem Geir Morten Egeberg
Petter Muren
Pål Hagh Sandberg
Original Assignee
Prox Dynamics As
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 Prox Dynamics As filed Critical Prox Dynamics As
Publication of SG11201405891PA publication Critical patent/SG11201405891PA/en

Links

Classifications

    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64C—AEROPLANES; HELICOPTERS
    • B64C19/00—Aircraft control not otherwise provided for
    • 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
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64C—AEROPLANES; HELICOPTERS
    • B64C27/00—Rotorcraft; Rotors peculiar thereto
    • B64C27/04—Helicopters
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64C—AEROPLANES; HELICOPTERS
    • B64C27/00—Rotorcraft; Rotors peculiar thereto
    • B64C27/54—Mechanisms for controlling blade adjustment or movement relative to rotor head, e.g. lag-lead movement
    • B64C27/56—Mechanisms for controlling blade adjustment or movement relative to rotor head, e.g. lag-lead movement characterised by the control initiating means, e.g. manually actuated
    • B64C27/57—Mechanisms for controlling blade adjustment or movement relative to rotor head, e.g. lag-lead movement characterised by the control initiating means, e.g. manually actuated automatic or condition responsive, e.g. responsive to rotor speed, torque or thrust

Landscapes

  • Engineering & Computer Science (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Mechanical 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)
  • Toys (AREA)
SG11201405891PA 2012-03-21 2013-02-27 Altitude regulator SG11201405891PA (en)

Applications Claiming Priority (3)

Application Number Priority Date Filing Date Title
US201261613720P 2012-03-21 2012-03-21
NO20120340A NO334600B1 (en) 2012-03-21 2012-04-12 Position control for rotary-wing aircraft
PCT/EP2013/053891 WO2013139567A1 (en) 2012-03-21 2013-02-27 Altitude regulator

Publications (1)

Publication Number Publication Date
SG11201405891PA true SG11201405891PA (en) 2014-10-30

Family

ID=49484502

Family Applications (1)

Application Number Title Priority Date Filing Date
SG11201405891PA SG11201405891PA (en) 2012-03-21 2013-02-27 Altitude regulator

Country Status (6)

Country Link
US (1) US8682506B2 (en)
EP (1) EP2828719B1 (en)
AU (1) AU2013234603B2 (en)
NO (1) NO334600B1 (en)
SG (1) SG11201405891PA (en)
WO (1) WO2013139567A1 (en)

Families Citing this family (15)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN103760906B (en) * 2014-01-29 2016-06-01 天津大学 Neural network and non-linear continuous depopulated helicopter attitude control method
CN103760905B (en) * 2014-01-29 2016-06-01 天津大学 Based on fuzzy feedforward list rotor unmanned helicopter attitude nonlinear robust control method
JP6207746B2 (en) 2014-05-30 2017-10-04 エスゼット ディージェイアイ テクノロジー カンパニー リミテッドＳｚ Ｄｊｉ Ｔｅｃｈｎｏｌｏｇｙ Ｃｏ．，Ｌｔｄ Aircraft attitude control method and apparatus
CN104155985B (en) * 2014-08-08 2015-05-20 北京航天自动控制研究所 Crosslinking impact assessment method for inertia coupling property between aircraft attitude movement channels
CN104155983B (en) * 2014-08-08 2015-05-20 北京航天自动控制研究所 Crosslinking impact assessment method for aerodynamic coupling property between aircraft attitude movement channels
WO2016053862A1 (en) * 2014-09-30 2016-04-07 Sikorsky Aircraft Corporation Torque and thrust control of a propeller
CN110062735B (en) 2016-12-22 2023-03-28 小鹰公司 Distributed flight control system
CN107357302A (en) * 2017-09-09 2017-11-17 郑州大学 The tumbling action implementation method and device of a kind of quadrotor
CN107908193B (en) * 2017-12-29 2024-02-09 福州大学 Non-planar eight-rotor omnidirectional aircraft and control method
US11092136B2 (en) * 2018-05-04 2021-08-17 Raytheon Technologies Corporation Systems and methods for optimal speed protection for power turbine governing
CN112650270A (en) * 2019-10-11 2021-04-13 天津工业大学 Motion model applied to unmanned aerial vehicle and model identification technology
US11435761B1 (en) 2021-07-23 2022-09-06 Beta Air, Llc System and method for distributed flight control system for an electric vehicle
US11427305B1 (en) 2021-09-16 2022-08-30 Beta Air, Llc Methods and systems for flight control for managing actuators for an electric aircraft
US11465734B1 (en) 2021-09-16 2022-10-11 Beta Air, Llc Systems and methods for distrubuted flight controllers for redundancy for an electric aircraft
CN113917937B (en) * 2021-09-29 2024-08-27 普宙科技有限公司 Multi-rotor-wing attitude active disturbance rejection control method and system based on shaft angle vector

Family Cites Families (14)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
GB671076A (en) 1948-10-14 1952-04-30 Sncaso Improvements in speed governors and their application to helicopters
US4648797A (en) 1983-12-19 1987-03-10 United Technologies Corporation Torque control system
GB8629896D0 (en) 1986-12-15 1987-01-28 Westland Plc Helicopter flight control system
US5169090A (en) 1991-08-28 1992-12-08 United Technologies Corporation Attitude synchronization for model following control systems
US5850615A (en) * 1995-12-06 1998-12-15 Mcdonnell Douglas Helicopter Co. Rotor blade swashplate-axis rotation and gyroscopic moments componsator
US6873887B2 (en) 2001-11-13 2005-03-29 Goodrich Pump & Engine Control Systems, Inc. Rotor torque anticipator
US6879885B2 (en) 2001-11-16 2005-04-12 Goodrich Pump & Engine Control Systems, Inc. Rotor torque predictor
US6751529B1 (en) 2002-06-03 2004-06-15 Neural Robotics, Inc. System and method for controlling model aircraft
WO2005100154A1 (en) 2004-04-13 2005-10-27 Wavefront Technology Pty Ltd System for rotor head and rotor blade
US7900869B2 (en) 2004-05-06 2011-03-08 Zf Friedrichshafen Ag Helicopter rotor control system with individual blade control
FR2876468B1 (en) 2004-10-08 2007-08-17 Eurocopter France AUTOMATIC HELICOPTER CONTROL SYSTEM
DE102005051799A1 (en) * 2005-10-27 2007-05-03 Stefan Reich Method and device for remote control and stabilization of unmanned aerial vehicles
US8694182B2 (en) * 2007-04-03 2014-04-08 Sikorsky Aircraft Corporation Altitude and acceleration command altitude hold algorithm for rotorcraft with large center of gravity range
US7970498B2 (en) 2007-06-01 2011-06-28 Sikorsky Aircraft Corporation Model based sensor system for loads aware control laws

Also Published As

Publication number Publication date
WO2013139567A1 (en) 2013-09-26
AU2013234603A1 (en) 2014-10-09
NO334600B1 (en) 2014-04-22
US8682506B2 (en) 2014-03-25
NO20120340A1 (en) 2013-09-23
AU2013234603B2 (en) 2016-06-09
US20130306787A1 (en) 2013-11-21
EP2828719B1 (en) 2019-03-13
EP2828719A1 (en) 2015-01-28

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