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
Other languages
English (en)
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 (no) 2012-03-21 2012-04-12 Stillingskontroll for roterende-vinge luftfartøy
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 (no)
EP (1) EP2828719B1 (no)
AU (1) AU2013234603B2 (no)
NO (1) NO334600B1 (no)
SG (1) SG11201405891PA (no)
WO (1) WO2013139567A1 (no)

Families Citing this family (13)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN103760906B (zh) * 2014-01-29 2016-06-01 天津大学 神经网络与非线性连续无人直升机姿态控制方法
CN103760905B (zh) * 2014-01-29 2016-06-01 天津大学 基于模糊前馈单旋翼无人直升机姿态非线性鲁棒控制方法
JP6207746B2 (ja) 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 航空機姿勢制御方法及び装置
CN104155985B (zh) * 2014-08-08 2015-05-20 北京航天自动控制研究所 飞行器姿态运动通道间惯性耦合特性的交联影响确定方法
CN104155983B (zh) * 2014-08-08 2015-05-20 北京航天自动控制研究所 飞行器姿态运动通道间气动耦合特性的交联影响确定方法
US10336436B2 (en) 2014-09-30 2019-07-02 Sikorsky Aircraft Corporation Torque and thrust control of a propeller
CN116069066A (zh) 2016-12-22 2023-05-05 小鹰公司 分布式飞行控制系统
CN107357302A (zh) * 2017-09-09 2017-11-17 郑州大学 一种四旋翼飞行器的翻滚动作实现方法和装置
CN107908193B (zh) * 2017-12-29 2024-02-09 福州大学 一种非平面式八旋翼全向飞行器及控制方法
US11092136B2 (en) * 2018-05-04 2021-08-17 Raytheon Technologies Corporation Systems and methods for optimal speed protection for power turbine governing
CN112650270A (zh) * 2019-10-11 2021-04-13 天津工业大学 一种应用在无人机上的运动模型与模型辨识技术
US11435761B1 (en) 2021-07-23 2022-09-06 Beta Air, Llc System and method for distributed flight control system for an electric vehicle
US11465734B1 (en) 2021-09-16 2022-10-11 Beta Air, Llc Systems and methods for distrubuted flight controllers for redundancy for an electric aircraft

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
WO2006134425A2 (en) 2004-05-06 2006-12-21 Zf Friedrichshafen Ag Helicopter rotor control system with individual blade control
FR2876468B1 (fr) 2004-10-08 2007-08-17 Eurocopter France Systeme de pilotage automatique d'un helicoptere
DE102005051799A1 (de) * 2005-10-27 2007-05-03 Stefan Reich Verfahren und Vorrichtung zur Fernsteuerung und Stabilisierung unbemannter Luftfahrzeuge
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
NO20120340A1 (no) 2013-09-23
EP2828719A1 (en) 2015-01-28
AU2013234603A1 (en) 2014-10-09
NO334600B1 (no) 2014-04-22
WO2013139567A1 (en) 2013-09-26
AU2013234603B2 (en) 2016-06-09
US8682506B2 (en) 2014-03-25
EP2828719B1 (en) 2019-03-13
US20130306787A1 (en) 2013-11-21

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