JP2018020759A5 - - Google Patents

Download PDF

Info

Publication number
JP2018020759A5
JP2018020759A5 JP2017089267A JP2017089267A JP2018020759A5 JP 2018020759 A5 JP2018020759 A5 JP 2018020759A5 JP 2017089267 A JP2017089267 A JP 2017089267A JP 2017089267 A JP2017089267 A JP 2017089267A JP 2018020759 A5 JP2018020759 A5 JP 2018020759A5
Authority
JP
Japan
Prior art keywords
change
rate
aerodynamic angle
inertial
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
JP2017089267A
Other languages
English (en)
Japanese (ja)
Other versions
JP2018020759A (ja
JP6737737B2 (ja
Filing date
Publication date
Priority claimed from US15/157,762 external-priority patent/US9910445B2/en
Application filed filed Critical
Publication of JP2018020759A publication Critical patent/JP2018020759A/ja
Publication of JP2018020759A5 publication Critical patent/JP2018020759A5/ja
Application granted granted Critical
Publication of JP6737737B2 publication Critical patent/JP6737737B2/ja
Active legal-status Critical Current
Anticipated expiration legal-status Critical

Links

JP2017089267A 2016-05-18 2017-04-28 航空機の空力角度のための適合フィルタリングシステム Active JP6737737B2 (ja)

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
US15/157,762 2016-05-18
US15/157,762 US9910445B2 (en) 2016-05-18 2016-05-18 Adaptive filtering system for aerodynamic angles of an aircraft

Publications (3)

Publication Number Publication Date
JP2018020759A JP2018020759A (ja) 2018-02-08
JP2018020759A5 true JP2018020759A5 (enExample) 2020-06-25
JP6737737B2 JP6737737B2 (ja) 2020-08-12

Family

ID=58709320

Family Applications (1)

Application Number Title Priority Date Filing Date
JP2017089267A Active JP6737737B2 (ja) 2016-05-18 2017-04-28 航空機の空力角度のための適合フィルタリングシステム

Country Status (6)

Country Link
US (1) US9910445B2 (enExample)
EP (1) EP3246712B1 (enExample)
JP (1) JP6737737B2 (enExample)
CN (1) CN107436607B (enExample)
BR (1) BR102017009774B1 (enExample)
RU (1) RU2735751C2 (enExample)

Families Citing this family (12)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US20190217966A1 (en) * 2018-01-12 2019-07-18 Rosemount Aerospace Inc. Aircraft air data generation using laser sensor data and inertial sensor data
US11066189B2 (en) 2018-12-07 2021-07-20 The Boeing Company Flight control system for determining estimated dynamic pressure based on lift and drag coefficients
US11003196B2 (en) * 2018-12-07 2021-05-11 The Boeing Company Flight control system for determining a common mode pneumatic fault
US11029706B2 (en) 2018-12-07 2021-06-08 The Boeing Company Flight control system for determining a fault based on error between a measured and an estimated angle of attack
US11186357B2 (en) * 2019-01-03 2021-11-30 Textron Innovations Inc. System and method for controlling rotorcraft
US12123894B2 (en) 2019-05-01 2024-10-22 Queen's University At Kingston Apparatus and method for measuring velocity perturbations in a fluid
USD902829S1 (en) * 2019-07-15 2020-11-24 Darold B Cummings Aircraft
USD941741S1 (en) * 2019-08-23 2022-01-25 Darold B Cummings Aircraft
JP7265260B2 (ja) * 2019-09-17 2023-04-26 国立研究開発法人宇宙航空研究開発機構 航空機
US12379730B2 (en) 2021-03-31 2025-08-05 Beta Air Llc Methods and systems for flight control configured for use in an electric aircraft
WO2023044173A2 (en) * 2021-09-17 2023-03-23 Beta Air, Llc Methods and systems for flight control configured for use in an electric aircraft
CN114878856B (zh) * 2022-04-15 2025-09-19 中国航空工业集团公司沈阳飞机设计研究所 一种表决后的真攻角与侧滑角滤波方法及系统

Family Cites Families (12)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US5170969A (en) * 1988-11-23 1992-12-15 The Boeing Company Aircraft rudder command system
US5669582A (en) 1995-05-12 1997-09-23 The Boeing Company Method and apparatus for reducing unwanted sideways motion in the aft cabin and roll-yaw upsets of an airplane due to atmospheric turbulence and wind gusts
US6273370B1 (en) 1999-11-01 2001-08-14 Lockheed Martin Corporation Method and system for estimation and correction of angle-of-attack and sideslip angle from acceleration measurements
US6711476B2 (en) * 2001-09-27 2004-03-23 The Boeing Company Method and computer program product for estimating at least one state of a dynamic system
US6928341B2 (en) * 2003-05-13 2005-08-09 The Boeing Company Computational air data system for angle-of-attack and angle-of-sideslip
EP2615026B1 (en) * 2011-06-10 2018-04-04 Airbus Defence and Space GmbH Method and apparatus for minimizing dynamic structural loads of an aircraft
FR2978858B1 (fr) * 2011-08-01 2013-08-30 Airbus Operations Sas Procede et systeme pour la determination de parametres de vol d'un aeronef
US9498903B2 (en) * 2012-10-31 2016-11-22 The Boeing Company System and method for manufacturing monolithic structures using expanding internal tools
RU2541902C2 (ru) * 2013-04-29 2015-02-20 Открытое акционерное общество "Лётно-исследовательский институт имени М.М. Громова" Интеллектуальная система поддержки экипажа
CN103926837B (zh) * 2014-04-22 2016-05-25 西北工业大学 多种耦合作用下飞行器综合解耦方法
CN103914074A (zh) * 2014-04-22 2014-07-09 西北工业大学 飞行器推力强耦合解耦方法
RU159568U1 (ru) * 2015-06-15 2016-02-10 Акционерное общество "Ульяновское конструкторское бюро приборостроения" (АО "УКБП") Система предупреждения критических режимов для маневренных самолетов

Similar Documents

Publication Publication Date Title
JP2018020759A5 (enExample)
US11041588B2 (en) Method and system for controlling a gimbal
RU2017109733A (ru) Система адаптивной фильтрации для аэродинамических углов летательного аппарата
JP2015526726A (ja) 風ベクトルの推定
AU2015213424B2 (en) Methods and apparatus to control aircraft horizontal stabilizers
JP6580325B2 (ja) 航空機の対気速度算出システム
RU2013139093A (ru) Система управления самолетом, самолет, программа управления самолетом и способ управления самолетом
RU2683718C2 (ru) Способ определения закона наведения для уклонения от препятствия летательным аппаратом, электронная система и летательный аппарат
CN108475069B (zh) 农业无人飞行器的控制方法、飞行控制器及农业无人机
US9684309B2 (en) Aircraft guidance based on partial differential equation for miss distance
EP3441306B1 (en) System and method for rotorcraft approach to hover
JP2018039390A5 (enExample)
CN104035445A (zh) 一种遥控装置、控制系统以及控制方法
US10099775B2 (en) Autopilot system for an aircraft and related process
CN105843232B (zh) 一种飞行器滑翔减速控制方法
JP4617990B2 (ja) 自動飛行制御装置、自動飛行制御方法及び自動飛行制御プログラム
US9889926B2 (en) Air vehicles and systems for preemptive turbulence mitigation
KR20150107662A (ko) 모듈화된 쿼드 로터 제어 시스템 및 그의 제어 방법
WO2018107733A1 (zh) 一种用于飞艇的控制方法和装置
Polivanov et al. Comparison of a quadcopter and an airplane as a means of measuring atmospheric parameters
Firsov et al. Compact vertical take-off and landing aerial vehicle for monitoring tasks in dense urban areas
CA2855284A1 (en) Flutter control actuator
Pedersini et al. Study and experimentation of control policies to dynamically maintain micro-UAV flight stability
Li et al. Research on Suspended Fire Fighting Robot Prototype
Limacher et al. On the Stable Leading Edge Vortex in Rotating Systems