IN2014MN01633A - - Google Patents
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- Publication number
- IN2014MN01633A IN2014MN01633A IN1633MUN2014A IN2014MN01633A IN 2014MN01633 A IN2014MN01633 A IN 2014MN01633A IN 1633MUN2014 A IN1633MUN2014 A IN 1633MUN2014A IN 2014MN01633 A IN2014MN01633 A IN 2014MN01633A
- Authority
- IN
- India
- Prior art keywords
- command
- eliminating
- vehicle
- miss distance
- reducing
- Prior art date
Links
- 230000001902 propagating effect Effects 0.000 abstract 1
Classifications
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F41—WEAPONS
- F41G—WEAPON SIGHTS; AIMING
- F41G7/00—Direction control systems for self-propelled missiles
- F41G7/20—Direction control systems for self-propelled missiles based on continuous observation of target position
- F41G7/22—Homing guidance systems
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F41—WEAPONS
- F41G—WEAPON SIGHTS; AIMING
- F41G7/00—Direction control systems for self-propelled missiles
- F41G7/20—Direction control systems for self-propelled missiles based on continuous observation of target position
- F41G7/30—Command link guidance systems
-
- 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
- G05D1/12—Target-seeking control
Landscapes
- Engineering & Computer Science (AREA)
- Chemical & Material Sciences (AREA)
- Combustion & Propulsion (AREA)
- General Engineering & Computer Science (AREA)
- Remote Sensing (AREA)
- Radar, Positioning & Navigation (AREA)
- Aviation & Aerospace Engineering (AREA)
- Physics & Mathematics (AREA)
- General Physics & Mathematics (AREA)
- Automation & Control Theory (AREA)
- Control Of Position, Course, Altitude, Or Attitude Of Moving Bodies (AREA)
- Steering Control In Accordance With Driving Conditions (AREA)
- Aiming, Guidance, Guns With A Light Source, Armor, Camouflage, And Targets (AREA)
Abstract
A system of providing guidance laws for maneuvering a vehicle for reducing or eliminating miss distance to a target including a system configured to provide a command for maneuvering the vehicle towards a target. The system is configured to repeatedly perform the following stages until eliminating the miss distance including: propagating vehicle s equation of motion as a result of the command while reducing or eliminating lack of consistency between the assumptions made to calculate the maneuver command and the actual performance when attempting to realize the command. Then calculating miss distance to the target and updating the command for reducing or eliminating the miss distance and sending the command to a steering system of the vehicle.
Applications Claiming Priority (2)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
IL217736A IL217736A (en) | 2012-01-26 | 2012-01-26 | Guidance laws for navigating vehicles |
PCT/IL2013/050070 WO2013111138A1 (en) | 2012-01-26 | 2013-01-24 | Guidance laws for navigating vehicles |
Publications (1)
Publication Number | Publication Date |
---|---|
IN2014MN01633A true IN2014MN01633A (en) | 2015-05-15 |
Family
ID=46467083
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
IN1633MUN2014 IN2014MN01633A (en) | 2012-01-26 | 2013-01-24 |
Country Status (4)
Country | Link |
---|---|
EP (1) | EP2807443B1 (en) |
IL (1) | IL217736A (en) |
IN (1) | IN2014MN01633A (en) |
WO (1) | WO2013111138A1 (en) |
Families Citing this family (4)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
WO2015189485A1 (en) * | 2014-06-13 | 2015-12-17 | Mbda France | Method and system for the terminal-phase guiding of an interceptor missile towards a mobile aerial target |
US10942013B2 (en) | 2018-08-31 | 2021-03-09 | Bae Systems Information And Electronic Systems Integration Inc. | Guidance, navigation and control for ballistic projectiles |
US11009316B2 (en) * | 2018-11-02 | 2021-05-18 | Bae Systems Information And Electronic Systems Integration Inc. | Multi-mode adaptive nonlinear trajectory shaping (NTS) guidance law |
IL277347A (en) * | 2020-09-14 | 2022-04-01 | C 2 V Line Ltd | Method and system for homing |
Family Cites Families (6)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US4494202A (en) * | 1982-09-22 | 1985-01-15 | General Dynamics, Pomona Division | Fourth order predictive, augmented proportional navigation system terminal guidance design with missile/target decoupling |
US4589610A (en) * | 1983-11-08 | 1986-05-20 | Westinghouse Electric Corp. | Guided missile subsystem |
US6006145A (en) | 1997-06-30 | 1999-12-21 | The United States Of America As Represented By The Secretary Of The Navy | Method and apparatus for directing a pursuing vehicle to a target with intelligent evasion capabilities |
US6845938B2 (en) | 2001-09-19 | 2005-01-25 | Lockheed Martin Corporation | System and method for periodically adaptive guidance and control |
US7487933B1 (en) | 2005-07-05 | 2009-02-10 | Chen Robert H | Homing missile guidance and estimation algorithms against advanced maneuvering targets |
US7394047B1 (en) | 2006-05-09 | 2008-07-01 | Lockheed Martin Corporation | Interceptor guidance for boost-phase missile defense |
-
2012
- 2012-01-26 IL IL217736A patent/IL217736A/en active IP Right Grant
-
2013
- 2013-01-24 IN IN1633MUN2014 patent/IN2014MN01633A/en unknown
- 2013-01-24 WO PCT/IL2013/050070 patent/WO2013111138A1/en active Application Filing
- 2013-01-24 EP EP13741598.0A patent/EP2807443B1/en active Active
Also Published As
Publication number | Publication date |
---|---|
EP2807443B1 (en) | 2021-03-10 |
WO2013111138A1 (en) | 2013-08-01 |
EP2807443A1 (en) | 2014-12-03 |
EP2807443A4 (en) | 2015-10-14 |
IL217736A0 (en) | 2012-06-28 |
IL217736A (en) | 2017-06-29 |
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