AU2001233902A1 - A ballistics fire control solution process and apparatus for a spin or fin stabilised projectile - Google Patents
A ballistics fire control solution process and apparatus for a spin or fin stabilised projectileInfo
- Publication number
- AU2001233902A1 AU2001233902A1 AU2001233902A AU3390201A AU2001233902A1 AU 2001233902 A1 AU2001233902 A1 AU 2001233902A1 AU 2001233902 A AU2001233902 A AU 2001233902A AU 3390201 A AU3390201 A AU 3390201A AU 2001233902 A1 AU2001233902 A1 AU 2001233902A1
- Authority
- AU
- Australia
- Prior art keywords
- projectile
- vector
- spin
- fire control
- control solution
- 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.)
- Abandoned
Links
Classifications
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F41—WEAPONS
- F41G—WEAPON SIGHTS; AIMING
- F41G3/00—Aiming or laying means
- F41G3/14—Indirect aiming means
- F41G3/142—Indirect aiming means based on observation of a first shoot; using a simulated shoot
Landscapes
- Engineering & Computer Science (AREA)
- General Engineering & Computer Science (AREA)
- Aiming, Guidance, Guns With A Light Source, Armor, Camouflage, And Targets (AREA)
- Radar Systems Or Details Thereof (AREA)
- Fire-Extinguishing By Fire Departments, And Fire-Extinguishing Equipment And Control Thereof (AREA)
- Organic Low-Molecular-Weight Compounds And Preparation Thereof (AREA)
- Catalysts (AREA)
- Control Of Position, Course, Altitude, Or Attitude Of Moving Bodies (AREA)
Abstract
A ballistics fire control system for a spin or fin stabilized projectile is provided with means which are operated such that the closest point of approach between a fired projectile and a target is taken to be at the instant the projectile velocity vector (6) is orthogonal to the position error vector (13) between the projectile and target in accordance with the relationship: Vp.(PP-PF)=0 where Vp is the projectile velocity vector, PP is the projectile trajectory or position vector, PF is the target future position vector, . is the vector dot product and (PP-PF) is the position error vector.
Applications Claiming Priority (3)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
GBGB0005594.7A GB0005594D0 (en) | 2000-03-09 | 2000-03-09 | A ballistics fire control solution process and apparatus for a spin or fin stabilised projectile |
GB0005594 | 2000-03-09 | ||
PCT/GB2001/000708 WO2001067025A2 (en) | 2000-03-09 | 2001-02-20 | A ballistics fire control solution process and apparatus for a spin or fin stabilised projectile |
Publications (1)
Publication Number | Publication Date |
---|---|
AU2001233902A1 true AU2001233902A1 (en) | 2001-09-17 |
Family
ID=9887224
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
AU2001233902A Abandoned AU2001233902A1 (en) | 2000-03-09 | 2001-02-20 | A ballistics fire control solution process and apparatus for a spin or fin stabilised projectile |
Country Status (8)
Country | Link |
---|---|
US (1) | US6776336B2 (en) |
EP (1) | EP1264154B1 (en) |
AT (1) | ATE349670T1 (en) |
AU (1) | AU2001233902A1 (en) |
DE (1) | DE60125515T2 (en) |
GB (1) | GB0005594D0 (en) |
IL (2) | IL151629A0 (en) |
WO (1) | WO2001067025A2 (en) |
Families Citing this family (4)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US7121183B2 (en) * | 2004-03-29 | 2006-10-17 | Honeywell International Inc. | Methods and systems for estimating weapon effectiveness |
DE102005041704A1 (en) * | 2005-09-02 | 2007-03-15 | Oerlikon Contraves Ag | Method for optimizing a fire triggering of a weapon or a gun |
US7417583B2 (en) * | 2006-10-30 | 2008-08-26 | Raytheon Company | Methods and apparatus for providing target altitude estimation in a two dimensional radar system |
CN111025351B (en) * | 2019-12-05 | 2021-11-30 | 中国人民解放军63620部队 | Real-time estimation method for time zero difference of carrier rocket navigation calculation and external measurement system |
Family Cites Families (16)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
GB233691A (en) | 1924-05-08 | 1926-07-27 | Anonima Edoardo Bianchi Soc | Improvements in steering or head tubes for cycles, motor cycles and the like vehicles |
US3230348A (en) * | 1951-09-01 | 1966-01-18 | Sperry Rand Corp | Missile guidance system |
US4128837A (en) * | 1968-07-22 | 1978-12-05 | Rockwell International Corporation | Prediction computation for weapon control |
US3737902A (en) * | 1970-08-19 | 1973-06-05 | State Street Bank & Trust Co | Collision avoidance system providing a vector signal representative of the distance and bearing between a prime vehicle and target object at a predicted closest point of approach therebetween |
US4124849A (en) * | 1970-12-30 | 1978-11-07 | Zahornasky Vincent T | Positioning system |
DE2614680A1 (en) * | 1975-04-07 | 1976-10-21 | Motorola Inc | METHOD AND APPARATUS FOR MEASURING THE VECTOR OF A MINIMUM HIT DEPOSIT |
US4146780A (en) * | 1976-12-17 | 1979-03-27 | Ares, Inc. | Antiaircraft weapons system fire control apparatus |
US5644099A (en) * | 1977-01-18 | 1997-07-01 | Telefunken Systemtechnik Gmbh | Proximity detonator |
FR2378318A1 (en) * | 1977-01-21 | 1978-08-18 | Thomson Csf | MOBILE TARGET TRACKING SYSTEM |
AU527407B2 (en) * | 1978-10-23 | 1983-03-03 | Australasian Training Aids Pty. Ltd. | Detecting the passing of an object |
US4312262A (en) * | 1979-02-22 | 1982-01-26 | General Electric Company | Relative velocity gunsight system and method |
DE3236206C1 (en) | 1982-09-30 | 1983-12-29 | Honeywell Gmbh, 6050 Offenbach | Procedure for determining the placement of the projectile impact on shooting simulators |
US4672381A (en) * | 1984-08-30 | 1987-06-09 | Paul Labbe | Doppler tracking processor and time of closest approach detector |
FR2577036B1 (en) * | 1985-01-31 | 1987-03-27 | France Etat Armement | PROJECTILE WEAPON SYSTEM CONTAINING A VULNERANT LOAD |
US5164910A (en) * | 1990-07-03 | 1992-11-17 | Martin Marietta Corporation | Moving target discrimination from passive measurements |
US5140329A (en) * | 1991-04-24 | 1992-08-18 | Lear Astronics Corporation | Trajectory analysis radar system for artillery piece |
-
2000
- 2000-03-09 GB GBGB0005594.7A patent/GB0005594D0/en not_active Ceased
-
2001
- 2001-02-20 WO PCT/GB2001/000708 patent/WO2001067025A2/en active IP Right Grant
- 2001-02-20 AT AT01905938T patent/ATE349670T1/en not_active IP Right Cessation
- 2001-02-20 AU AU2001233902A patent/AU2001233902A1/en not_active Abandoned
- 2001-02-20 EP EP01905938A patent/EP1264154B1/en not_active Expired - Lifetime
- 2001-02-20 US US10/220,804 patent/US6776336B2/en not_active Expired - Fee Related
- 2001-02-20 DE DE60125515T patent/DE60125515T2/en not_active Expired - Lifetime
- 2001-02-20 IL IL15162901A patent/IL151629A0/en active IP Right Grant
-
2002
- 2002-09-05 IL IL151629A patent/IL151629A/en not_active IP Right Cessation
Also Published As
Publication number | Publication date |
---|---|
US6776336B2 (en) | 2004-08-17 |
ATE349670T1 (en) | 2007-01-15 |
DE60125515D1 (en) | 2007-02-08 |
GB0005594D0 (en) | 2000-12-20 |
IL151629A (en) | 2007-03-08 |
US20030141364A1 (en) | 2003-07-31 |
WO2001067025A2 (en) | 2001-09-13 |
EP1264154A2 (en) | 2002-12-11 |
DE60125515T2 (en) | 2007-10-04 |
EP1264154B1 (en) | 2006-12-27 |
WO2001067025A3 (en) | 2002-03-14 |
IL151629A0 (en) | 2003-04-10 |
Similar Documents
Publication | Publication Date | Title |
---|---|---|
US5425514A (en) | Modular aerodynamic gyrodynamic intelligent controlled projectile and method of operating same | |
EP0752573A3 (en) | Missile fuzing system | |
EP0131573B1 (en) | Ram air combustion steering system for a guided missile | |
WO1996025641A3 (en) | Method and apparatus for radial thrust trajectory correction of a ballistic projectile | |
AU2001277489A1 (en) | Radar device for object self-protection | |
WO2006079029A3 (en) | Defense system and method | |
US4198015A (en) | Ideal trajectory shaping for anti-armor missiles via time optimal controller autopilot | |
AU2001233902A1 (en) | A ballistics fire control solution process and apparatus for a spin or fin stabilised projectile | |
AU3981885A (en) | Weapon system and missile for the structural destruction of an aerial target by means of a focussed charge | |
NO156263B (en) | DEVICE FOR DIRECTIONAL MANAGEMENT OF A PROJECT. | |
EP0747655A3 (en) | Blended missile autopilot | |
EP1298408A3 (en) | Improved direction infrared counter measure | |
SG127710A1 (en) | Method for programming the shattering of projectiles and tube weapon with programming system | |
EP0261091A3 (en) | A method and an apparatus for tracking a missile in its trajectory | |
ES8202141A1 (en) | Method of compensation for target location changes when firing ballistic missiles | |
AU2002221244A1 (en) | Method for controlling a missile | |
GB2177213A (en) | Determining the ballistic trajectory of a projectile | |
Champigny | High angle of attack aerodynamics | |
Zeng et al. | Cooperative salvo attack using guidance law of multiple missiles | |
SE8404402D0 (en) | SET AND DEVICE FOR REDUCING MAGNETIC SIGNATURE FOR GREAT SHIPPING DETAILS | |
GB0012119D0 (en) | Shell for defence against an approaching kinetic-energy projectile | |
Takano et al. | On an Air-to-Sea Guided Bomb | |
GB2251834A (en) | Guided missiles and like devices | |
Whang et al. | A LOS Rate Estimator for Homing Seekers with 2 Axis Gimbal System | |
JPH01239398A (en) | Missile guiding device |