IL136870A - Compensation for rotorcraft pitch axis control saturation - Google Patents
Compensation for rotorcraft pitch axis control saturationInfo
- Publication number
- IL136870A IL136870A IL13687098A IL13687098A IL136870A IL 136870 A IL136870 A IL 136870A IL 13687098 A IL13687098 A IL 13687098A IL 13687098 A IL13687098 A IL 13687098A IL 136870 A IL136870 A IL 136870A
- Authority
- IL
- Israel
- Prior art keywords
- servo command
- command signal
- unlimited
- pitch
- collective
- Prior art date
Links
- 230000003750 conditioning effect Effects 0.000 claims abstract description 18
- 230000004044 response Effects 0.000 claims description 26
- 238000007493 shaping process Methods 0.000 claims description 20
- 239000011295 pitch Substances 0.000 description 88
- 125000004122 cyclic group Chemical group 0.000 description 7
- 238000012545 processing Methods 0.000 description 7
- RZVHIXYEVGDQDX-UHFFFAOYSA-N 9,10-anthraquinone Chemical compound C1=CC=C2C(=O)C3=CC=CC=C3C(=O)C2=C1 RZVHIXYEVGDQDX-UHFFFAOYSA-N 0.000 description 6
- 230000009467 reduction Effects 0.000 description 6
- 238000010586 diagram Methods 0.000 description 5
- 238000013459 approach Methods 0.000 description 4
- 230000008859 change Effects 0.000 description 4
- 238000004891 communication Methods 0.000 description 4
- 230000001965 increasing effect Effects 0.000 description 4
- 230000006872 improvement Effects 0.000 description 3
- 230000002829 reductive effect Effects 0.000 description 3
- 230000009471 action Effects 0.000 description 2
- 230000002411 adverse Effects 0.000 description 2
- 238000012937 correction Methods 0.000 description 2
- 230000001351 cycling effect Effects 0.000 description 2
- 230000003247 decreasing effect Effects 0.000 description 2
- 230000000694 effects Effects 0.000 description 2
- 238000000034 method Methods 0.000 description 2
- 230000003466 anti-cipated effect Effects 0.000 description 1
- 230000002238 attenuated effect Effects 0.000 description 1
- 230000008901 benefit Effects 0.000 description 1
- JLQUFIHWVLZVTJ-UHFFFAOYSA-N carbosulfan Chemical compound CCCCN(CCCC)SN(C)C(=O)OC1=CC=CC2=C1OC(C)(C)C2 JLQUFIHWVLZVTJ-UHFFFAOYSA-N 0.000 description 1
- 230000007423 decrease Effects 0.000 description 1
- 238000013461 design Methods 0.000 description 1
- 238000011161 development Methods 0.000 description 1
- 230000002708 enhancing effect Effects 0.000 description 1
- 230000000670 limiting effect Effects 0.000 description 1
- 238000012544 monitoring process Methods 0.000 description 1
- 230000010355 oscillation Effects 0.000 description 1
- 230000002035 prolonged effect Effects 0.000 description 1
- 238000012360 testing method Methods 0.000 description 1
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
- G05D1/0011—Control of position, course, altitude or attitude of land, water, air or space vehicles, e.g. using automatic pilots associated with a remote control arrangement
- G05D1/0033—Control of position, course, altitude or attitude of land, water, air or space vehicles, e.g. using automatic pilots associated with a remote control arrangement by having the operator tracking the vehicle either by direct line of sight or via one or more cameras located remotely from the vehicle
-
- 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
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)
- Feedback Control In General (AREA)
- Control Of Position, Course, Altitude, Or Attitude Of Moving Bodies (AREA)
Applications Claiming Priority (2)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| US08/996,692 US5971325A (en) | 1997-12-23 | 1997-12-23 | Compensation for rotorcraft pitch axis control saturation |
| PCT/US1998/025869 WO1999032951A1 (en) | 1997-12-23 | 1998-12-04 | Compensation for rotorcraft pitch axis control saturation |
Publications (2)
| Publication Number | Publication Date |
|---|---|
| IL136870A0 IL136870A0 (en) | 2001-06-14 |
| IL136870A true IL136870A (en) | 2004-06-20 |
Family
ID=25543196
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| IL13687098A IL136870A (en) | 1997-12-23 | 1998-12-04 | Compensation for rotorcraft pitch axis control saturation |
Country Status (8)
| Country | Link |
|---|---|
| US (1) | US5971325A (de) |
| EP (1) | EP1042707B1 (de) |
| JP (1) | JP2001526997A (de) |
| AU (1) | AU747638B2 (de) |
| CA (1) | CA2316244A1 (de) |
| DE (1) | DE69804859T2 (de) |
| IL (1) | IL136870A (de) |
| WO (1) | WO1999032951A1 (de) |
Families Citing this family (15)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| FR2808339B1 (fr) * | 2000-04-26 | 2003-06-13 | Valeo Electronique | Vehicule, en particulier vehicule automobile, equipe d'un systeme permettant de commander un ouvrant a distance et systeme permettant la realisation d'une telle commande |
| ATE305150T1 (de) | 2000-05-17 | 2005-10-15 | Boeing Co | Intuitives fahrzeug und maschinensteuerung |
| US6648269B2 (en) | 2001-12-10 | 2003-11-18 | Sikorsky Aircraft Corporation | Trim augmentation system for a rotary wing aircraft |
| US6694228B2 (en) | 2002-05-09 | 2004-02-17 | Sikorsky Aircraft Corporation | Control system for remotely operated vehicles for operational payload employment |
| US6774860B2 (en) * | 2002-05-15 | 2004-08-10 | Northrop Grumman Corporation | UAV (unmanned air vehicle) servoing dipole |
| US7463956B2 (en) * | 2003-07-03 | 2008-12-09 | The Boeing Company | Constant vertical state maintaining cueing system |
| FR2876468B1 (fr) * | 2004-10-08 | 2007-08-17 | Eurocopter France | Systeme de pilotage automatique d'un helicoptere |
| US7642975B2 (en) * | 2008-03-12 | 2010-01-05 | Sikorsky Aircraft Corporation | Frame assembly for electrical bond |
| US9317042B2 (en) * | 2014-01-28 | 2016-04-19 | Sikorsky Aircraft Corporation | Pitch feedback control splitting for helicopters with redundant actuators |
| US10488870B2 (en) | 2015-04-16 | 2019-11-26 | Sikorsky Aircraft Corporation | Gust alleviating control for a coaxial rotary wing aircraft |
| US10144504B1 (en) * | 2017-09-01 | 2018-12-04 | Kitty Hawk Corporation | Decoupled hand controls for aircraft with vertical takeoff and landing and forward flight capabilities |
| CN110187634B (zh) * | 2018-02-23 | 2023-01-31 | 北京京东乾石科技有限公司 | 飞行器的控制方法、装置和计算机可读存储介质 |
| US11092136B2 (en) * | 2018-05-04 | 2021-08-17 | Raytheon Technologies Corporation | Systems and methods for optimal speed protection for power turbine governing |
| WO2020068666A1 (en) * | 2018-09-24 | 2020-04-02 | Dolby Laboratories Licensing Corporation | Image denoising in sdr to hdr image conversion |
| US20240239531A1 (en) * | 2022-08-09 | 2024-07-18 | Pete Bitar | Compact and Lightweight Drone Delivery Device called an ArcSpear Electric Jet Drone System Having an Electric Ducted Air Propulsion System and Being Relatively Difficult to Track in Flight |
Family Cites Families (10)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| JPS5515359B2 (de) * | 1974-11-22 | 1980-04-23 | ||
| US4071811A (en) * | 1976-03-01 | 1978-01-31 | Arlyle Floyd Irwin | Model helicopter throttle governor/collective pitch control apparatus |
| US4032083A (en) * | 1976-04-12 | 1977-06-28 | United Technologies Corporation | Automatic gain control for stability augmentation systems |
| US4420808A (en) * | 1980-04-01 | 1983-12-13 | United Technologies Corporation | Multi-axis force stick, self-trimmed aircraft flight control system |
| US4628455A (en) * | 1983-05-06 | 1986-12-09 | Sperry Corporation | Cross axis torque limiter for helicopter autopilot |
| US5058824A (en) * | 1989-12-21 | 1991-10-22 | United Technologies Corporation | Servo control system for a co-axial rotary winged aircraft |
| US5152478A (en) * | 1990-05-18 | 1992-10-06 | United Technologies Corporation | Unmanned flight vehicle including counter rotating rotors positioned within a toroidal shroud and operable to provide all required vehicle flight controls |
| EP0601000B1 (de) * | 1991-08-28 | 1997-01-29 | United Technologies Corporation | System zur vertikalen steuerung für drehflügelflugzeug |
| US5552983A (en) * | 1994-03-02 | 1996-09-03 | United Technologies Corporation | Variable referenced control system for remotely operated vehicles |
| US5429089A (en) * | 1994-04-12 | 1995-07-04 | United Technologies Corporation | Automatic engine speed hold control system |
-
1997
- 1997-12-23 US US08/996,692 patent/US5971325A/en not_active Expired - Lifetime
-
1998
- 1998-12-04 DE DE69804859T patent/DE69804859T2/de not_active Expired - Fee Related
- 1998-12-04 CA CA002316244A patent/CA2316244A1/en not_active Abandoned
- 1998-12-04 IL IL13687098A patent/IL136870A/en not_active IP Right Cessation
- 1998-12-04 AU AU18056/99A patent/AU747638B2/en not_active Ceased
- 1998-12-04 JP JP2000525799A patent/JP2001526997A/ja active Pending
- 1998-12-04 WO PCT/US1998/025869 patent/WO1999032951A1/en active IP Right Grant
- 1998-12-04 EP EP98962922A patent/EP1042707B1/de not_active Expired - Lifetime
Also Published As
| Publication number | Publication date |
|---|---|
| AU1805699A (en) | 1999-07-12 |
| JP2001526997A (ja) | 2001-12-25 |
| AU747638B2 (en) | 2002-05-16 |
| EP1042707B1 (de) | 2002-04-10 |
| DE69804859T2 (de) | 2002-11-28 |
| US5971325A (en) | 1999-10-26 |
| WO1999032951A1 (en) | 1999-07-01 |
| CA2316244A1 (en) | 1999-07-01 |
| DE69804859D1 (de) | 2002-05-16 |
| IL136870A0 (en) | 2001-06-14 |
| EP1042707A1 (de) | 2000-10-11 |
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Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| FF | Patent granted | ||
| KB | Patent renewed | ||
| MM9K | Patent not in force due to non-payment of renewal fees |