DE69307536D1 - Integrierte flugsteuerung und feuerleitanlage mit koordinierter bombenangriffsteuerung - Google Patents
Integrierte flugsteuerung und feuerleitanlage mit koordinierter bombenangriffsteuerungInfo
- Publication number
- DE69307536D1 DE69307536D1 DE69307536T DE69307536T DE69307536D1 DE 69307536 D1 DE69307536 D1 DE 69307536D1 DE 69307536 T DE69307536 T DE 69307536T DE 69307536 T DE69307536 T DE 69307536T DE 69307536 D1 DE69307536 D1 DE 69307536D1
- Authority
- DE
- Germany
- Prior art keywords
- control
- coordinated
- fire
- integrated flight
- bomb attack
- 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 - Fee Related
Links
- RZVHIXYEVGDQDX-UHFFFAOYSA-N 9,10-anthraquinone Chemical compound C1=CC=C2C(=O)C3=CC=CC=C3C(=O)C2=C1 RZVHIXYEVGDQDX-UHFFFAOYSA-N 0.000 title 1
Classifications
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64C—AEROPLANES; HELICOPTERS
- B64C13/00—Control systems or transmitting systems for actuating flying-control surfaces, lift-increasing flaps, air brakes, or spoilers
- B64C13/24—Transmitting means
- B64C13/38—Transmitting means with power amplification
- B64C13/50—Transmitting means with power amplification using electrical energy
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F41—WEAPONS
- F41G—WEAPON SIGHTS; AIMING
- F41G3/00—Aiming or laying means
- F41G3/22—Aiming or laying means for vehicle-borne armament, e.g. on aircraft
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F41—WEAPONS
- F41G—WEAPON SIGHTS; AIMING
- F41G5/00—Elevating or traversing control systems for guns
- F41G5/14—Elevating or traversing control systems for guns for vehicle-borne guns
- F41G5/18—Tracking systems for guns on aircraft
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F41—WEAPONS
- F41G—WEAPON SIGHTS; AIMING
- F41G9/00—Systems for controlling missiles or projectiles, not provided for elsewhere
- F41G9/002—Systems for controlling missiles or projectiles, not provided for elsewhere for guiding a craft to a correct firing position
-
- 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)
- General Engineering & Computer Science (AREA)
- Automation & Control Theory (AREA)
- Radar, Positioning & Navigation (AREA)
- Remote Sensing (AREA)
- Physics & Mathematics (AREA)
- General Physics & Mathematics (AREA)
- Aiming, Guidance, Guns With A Light Source, Armor, Camouflage, And Targets (AREA)
- Control Of Position, Course, Altitude, Or Attitude Of Moving Bodies (AREA)
Applications Claiming Priority (2)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
US07/967,308 US5310135A (en) | 1992-10-28 | 1992-10-28 | Helicopter integrated fire and flight control having coordinated area bombing control |
PCT/US1993/009500 WO1994010616A1 (en) | 1992-10-28 | 1993-10-05 | Helicopter integrated fire and flight control having coordinated area bombing control |
Publications (2)
Publication Number | Publication Date |
---|---|
DE69307536D1 true DE69307536D1 (de) | 1997-02-27 |
DE69307536T2 DE69307536T2 (de) | 1997-04-30 |
Family
ID=25512610
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
DE69307536T Expired - Fee Related DE69307536T2 (de) | 1992-10-28 | 1993-10-05 | Integrierte flugsteuerung und feuerleitanlage mit koordinierter bombenangriffsteuerung |
Country Status (5)
Country | Link |
---|---|
US (1) | US5310135A (de) |
EP (1) | EP0667005B1 (de) |
CA (1) | CA2144453C (de) |
DE (1) | DE69307536T2 (de) |
WO (1) | WO1994010616A1 (de) |
Families Citing this family (13)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
JP3166703B2 (ja) * | 1998-03-27 | 2001-05-14 | 双葉電子工業株式会社 | 遠隔制御ヘリコプタ用ジャイロ装置 |
US6145428A (en) * | 1998-03-31 | 2000-11-14 | Sikorsky Aircraft Corporation | Integrated fire and flight control system for controlling the angle of attack of a rotary wing aircraft |
US6012676A (en) * | 1998-03-31 | 2000-01-11 | Sikorsky Aircraft Corporation | Integrated fire and flight control system with automatic engine torque limiting |
US6648269B2 (en) * | 2001-12-10 | 2003-11-18 | Sikorsky Aircraft Corporation | Trim augmentation system for a rotary wing aircraft |
US20040059474A1 (en) * | 2002-09-20 | 2004-03-25 | Boorman Daniel J. | Apparatuses and methods for displaying autoflight information |
US7188007B2 (en) * | 2003-12-24 | 2007-03-06 | The Boeing Company | Apparatuses and methods for displaying and receiving tactical and strategic flight guidance information |
US8180562B2 (en) * | 2008-06-04 | 2012-05-15 | The Boeing Company | System and method for taxi route entry parsing |
US8386167B2 (en) * | 2008-11-14 | 2013-02-26 | The Boeing Company | Display of taxi route control point information |
CN102353301B (zh) * | 2011-09-15 | 2014-07-02 | 北京理工大学 | 基于虚拟目标点的带有终端约束的导引方法 |
US20160305740A1 (en) * | 2013-12-13 | 2016-10-20 | Profense, Llc | Gun Control Unit with Computerized Multi-Function Display |
US10508887B2 (en) | 2016-06-02 | 2019-12-17 | Sikorsky Aircraft Corporation | Attitude-coupled targeting system for rotary wing aircraft |
CN107878739B (zh) * | 2016-09-29 | 2020-12-22 | 北京理工大学 | 一种无人直升机控制系统及其控制方法 |
CN114740874B (zh) * | 2022-03-22 | 2024-07-12 | 西安爱生技术集团有限公司 | 无人机火箭助推发射滚转姿态控制方法 |
Family Cites Families (5)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US2933980A (en) * | 1953-08-03 | 1960-04-26 | North American Aviation Inc | Integrated aircraft and fire control autopilot |
US4067517A (en) * | 1976-02-03 | 1978-01-10 | United Technologies Corporation | Automatic heading synchronization control system |
FR2514487A1 (fr) * | 1981-10-14 | 1983-04-15 | Aerospatiale | Systeme de conduite de tir pour une arme de tir tendu montee sur un aeronef a voilure tournante |
US5096146A (en) * | 1990-08-17 | 1992-03-17 | The Boeing Company | Apparatus and methods for controlling commanded operation of an aircraft within a predetermined flight parameter limit |
US5222691A (en) * | 1991-08-28 | 1993-06-29 | United Technologies Corporation | Automatic turn coordination trim control for rotary wing aircraft |
-
1992
- 1992-10-28 US US07/967,308 patent/US5310135A/en not_active Expired - Lifetime
-
1993
- 1993-10-05 DE DE69307536T patent/DE69307536T2/de not_active Expired - Fee Related
- 1993-10-05 WO PCT/US1993/009500 patent/WO1994010616A1/en active IP Right Grant
- 1993-10-05 CA CA002144453A patent/CA2144453C/en not_active Expired - Fee Related
- 1993-10-05 EP EP93924913A patent/EP0667005B1/de not_active Expired - Lifetime
Also Published As
Publication number | Publication date |
---|---|
US5310135A (en) | 1994-05-10 |
CA2144453A1 (en) | 1994-05-11 |
WO1994010616A1 (en) | 1994-05-11 |
DE69307536T2 (de) | 1997-04-30 |
CA2144453C (en) | 2001-07-24 |
EP0667005A1 (de) | 1995-08-16 |
EP0667005B1 (de) | 1997-01-15 |
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Legal Events
Date | Code | Title | Description |
---|---|---|---|
8364 | No opposition during term of opposition | ||
8339 | Ceased/non-payment of the annual fee |