[특허]Missile director

Missile director 원문보기

IPC분류정보
국가/구분	United States(US) Patent 등록
국제특허분류(IPC7판)	F41G-001/46 F42B-015/10 G02B-027/00
출원번호	US-0569445 (1975-04-18)
발명자 / 주소	Esker Andrew T. (Florissant MO) Manche John L. (Bridgeton MO) Siler Robert M. (Anaheim CA)
출원인 / 주소	McDonnell Douglas Corporation (St. Louis MO 02)
인용정보	피인용 횟수 : 60 인용 특허 : 0

초록 ▼

A line of sight guidance system is provided in which the radiated output of a pulsed laser is spatially modulated to produce a beam radiated from an optical projector containing all informational requirements to enable a missile launched into the beam to determine its position with respect to beam center. The guidance system includes a single beam projector at a launch site, and a single beam receiver and signal decoder carried by the missile. The beam projector includes a laser diode source, laser pulse driver circuits, beam encoder, optic means for projecting the encoded beam, and electronic circuits for controlling the optic means operation. The beam encoder includes a reticle having a plurality of spokes formed in it, an opto-interrupter for sensing reticle center rotation rate, and drive motor control electronics. The reticle has a center mounted for rotation about the generated beam so that at least a portion of the reticle intersects the beam in all positions of the reticle. The laser diode source is pulsed at two different rates, which rates are coordinated with the angular position of the reticle. The laser beam is encoded by rotating the center of the reticle about an axis of the optical system in conjunction with the variation of the pulse repetition rate of the laser source, to produce a spatial modulation of the radiated beam. The projected beam, consequently, is a binary coded coordinate grid and reference data pattern which contains in itself all of the magnitude and phase components necessary for a properly equipped missile to define its location with respect to the beam coordinate center, once the missile is launched into the beam pattern. The receiver and decoder are utilized to derive signals for positioning the missile along the beam center by separating the incoming pulse train into an information channel and a phase reference channel. The optic means for projecting the beam includes a zoom optic system designed to permit use of a low power beam, the beam radiation being spread over a large angle at missile launch. The beam angle is decreased as the missile flies towards a target, thus maintaining approximately constant beam power density at the missile throughout flight, while minimizing the beam power density at the target.

대표청구항 ▼

A guidance system for directing the maneuvers of a guided device, comprising: a single radiated beam source of producing a single radiated beam; means for projecting said radiated beam along a first axis; a reticle having the center of rotation positioned along a second axis, said reticle having a pluralitY of spokes extending outwardly from said reticle center, said reticle center being mounted for rotation about said first axis, said reticle being rotatable about said second axis, at least a portion of said reticle intersecting said beam during rotation of said reticle about said first axis and said reticle about said second axis; means for rotating said reticle about said second axis at a first rotational speed; means for orbitally rotating the reticle center about said first axis at a second rotational speed; means for sequentially pulsing said single radiated beam source at a first rate during a first portion of one complete orbital revolution of said reticle center about said first axis, and for pulsing the single radiated beam source at a second rate during a second portion of one complete orbital revolution of said reticle center about said first axis; means carried by said guided device for receiving the beam input from said radiated beam source; and decoding means for providing information contained in said beam for positioning said device, said decoding means being operatively connected to said receiving means in said guided device, the information in said beam including distance and direction representations for permitting said guided device to determine a correction course to align itself with said first axis.

이 특허를 인용한 특허 (60)

Smith, Kirby A., Aimpoint offset countermeasures for area protection.
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Sammut, Dennis J., Apparatus and method for aiming point calculation.
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Sammut, Dennis J., Apparatus and method for aiming point calculation.
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Sammut, Dennis J., Apparatus and method for aiming point calculation.
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Sammut, Dennis J.; Buell, Dickinson; Chao, Lawrence, Apparatus and method for calculating aiming point information.
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Sammut, Dennis J.; Buell, Dickinson; Chao, Lawrence, Apparatus and method for calculating aiming point information.
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Sammut, Dennis J.; Buell, Dickinson; Chao, Lawrence, Apparatus and method for calculating aiming point information.
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Sammut, Dennis J.; Chao, Lawrence, Apparatus and method for calculating aiming point information.
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Sammut, Dennis J.; Chao, Lawrence, Apparatus and method for calculating aiming point information.
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Sammut, Dennis J.; Chao, Lawrence, Apparatus and method for calculating aiming point information.
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Sammut, Dennis J.; Chao, Lawrence, Apparatus and method for calculating aiming point information.
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Sammut, Dennis J.; Chao, Lawrence, Apparatus and method for calculating aiming point information.
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Sammut, Dennis J.; Chao, Lawrence; Buell, Dickinson, Apparatus and method for calculating aiming point information.
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Sammut, Dennis J.; Hodnett, Todd, Apparatus and method for calculating aiming point information.
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Sammut, Dennis J.; Hodnett, Todd, Apparatus and method for calculating aiming point information.
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Sammut, Dennis J.; Hodnett, Todd, Apparatus and method for calculating aiming point information.
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Sammut, Dennis J.; Hodnett, Todd, Apparatus and method for calculating aiming point information.
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Sammut, Dennis J.; Hodnett, Todd, Apparatus and method for calculating aiming point information.
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Sammut, Dennis; Hodnett, Todd, Apparatus and method for calculating aiming point information.
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Sammut, Dennis; Hodnett, Todd, Apparatus and method for calculating aiming point information.
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Sammut, Dennis; Hodnett, Todd, Apparatus and method for calculating aiming point information.
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Sammut, Dennis; Hodnett, Todd, Apparatus and method for calculating aiming point information.
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Sammut, Dennis; Hodnett, Todd, Apparatus and method for calculating aiming point information.
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Sammut, Dennis J.; Buell, Dickinson, Apparatus and method for calculating aiming point information for rifle scopes.
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Cremosnik Gregor (Regensdorf CHX) Timper Joachim (Zrich CHX) Holzberger Johann (Schfflisdorf CHX), Apparatus for guiding a missile.
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Tubb, G. David, Ballistic effect compensating reticle and aim compensation method.
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Tubb, G. David, Ballistic effect compensating reticle and aim compensation method.
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Tubb, G. David, Ballistic effect compensating reticle and aim compensation method with leveling reference and spin-drift compensated wind dots.
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Tubb, G. David, Ballistic effect compensating reticle and aim compensation method with sloped mil and MOA wind dot lines.
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Tubb, G. David, Ballistic effect compensating reticle, aim compensation method and adaptive method for compensating for variations in ammunition or variations in atmospheric conditions.
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McDonald, William True; Almgren, Ted C., Ballistic ranging methods and systems for inclined shooting.
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McDonald, William True; Almgren, Ted C., Ballistic ranging methods and systems for inclined shooting.
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Tong Kay C. (Mission Viejo CA), Beam-rider guidance using two overlapping reticle discs.
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Layton Allen C. (Orlando FL), Beamrider guidance technique using digital FM coding.
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Lindgren, Mikael, Device and method for a sight.
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Wes James A. (Diamond Bar CA) Ottoson Raymond H. (Garden Grove CA), Device to spatially encode a beam of light.
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Tubb, G. David, Dynamic targeting system with projectile-specific aiming indicia in a reticle and method for estimating ballistic effects of changing environment and ammunition.
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Tubb, G. David, Dynamic targeting system with projectile-specific aiming indicia in a reticle and method for estimating ballistic effects of changing environment and ammunition.
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Miles Perry A. (Lexington MA), Fire control system.
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Montgomery William J. (Antrim GB5) Nicholson Eric (Bangor GB5), Flight control apparatus.
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Diehl Christian (Munich DEX) Schnaebele Werner (Wolfratshausen DEX) Allgaier Karl-Heinz (Ottobrunn DEX) Kirsche Horst (Munich DEX), Guide beam and tracking system.
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Dennis J. Sammut, Gunsight and reticle therefor.
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Sammut Dennis J., Gunsight and reticle therefor.
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Sammut Dennis J., Gunsight and reticle therefor.
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Sammut, Dennis J., Gunsight and reticle therefor.
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Fendt Alfred (Munich DEX), Method and apparatus for measuring the optical axis of a guide beam projector.
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Seidensticker, Jens, Method for correcting the trajectory of a projectile, in particular of a terminal phase-guided projectile, and projectile for carrying out the method.
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Esker Andrew T. (St. Louis County MO), Missile director with beam axis shift capability.
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Hosaka Naoki,JPX ; Honda Hajime,JPX, Offset detection apparatus and flying object guiding system using the apparatus.
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Malueg Richard M. (Glendora CA), Optical image stabilizing system.
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Horwath Tibor G., Reticle for use in a guidance seeker for a spinning projectile.
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Tibor G. Horwath, Reticle for use in a guidance seeker for a spinning projectile.
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Mitchell Robert R. ; Miller Walter E., Retro-encoded missile guidance system.
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Henderson David M. (Playa Del Rey CA), Spatial coding of laser beams by optically biasing electro-optic modulators.
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Dunn, Albert; Ransom, Richard Sutton, Steering of missiles.
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Koreicho Wladimir (Chilly Mazarin FRX), System for guiding a missile by light beam.
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Chavany Jean C. (Chatenay-Malabry FRX) Koreicho Wladimir (Chilly-Mazarin FRX), System for guiding a missile by modulated light beam.
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Sogo Hiroshi (Utsunomiya JPX) Yoshino Nobuo (Utsunomiya JPX), System for guiding flying vehicles with light beam.
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Sogo Hiroshi (Utsunomiya JPX) Yoshino Nobuo (Utsunomiya JPX), System for guiding flying vehicles with light beam.
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Mitchell Robert R. (Huntsville AL), Tone burst reticle beamrider missile guidance.
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IPC	Description
A	생활필수품
A62	인명구조; 소방(사다리 E06C)
A62B	인명구조용의 기구, 장치 또는 방법(특히 의료용에 사용되는 밸브 A61M 39/00; 특히 물에서 쓰이는 인명구조 장치 또는 방법 B63C 9/00; 잠수장비 B63C 11/00; 특히 항공기에 쓰는 것, 예. 낙하산, 투출좌석 B64D; 특히 광산에서 쓰이는 구조장치 E21F 11/00)
A62B-1/08	.. 윈치 또는 풀리에 제동기구가 있는 것

내보내기 구분	파일저장 인쇄 메일전송
구성항목	기본정보 상세정보 관리번호, 국가코드, 자료구분, 상태, 출원번호, 출원일자, 공개번호, 공개일자, 등록번호, 등록일자, 발명명칭(한글), 발명명칭(영문), 출원인(한글), 출원인(영문), 출원인코드, 대표IPC 관리번호, 국가코드, 자료구분, 상태, 출원번호, 출원일자, 공개번호, 공개일자, 공고번호, 공고일자, 등록번호, 등록일자, 발명명칭(한글), 발명명칭(영문), 출원인(한글), 출원인(영문), 출원인코드, 대표출원인, 출원인국적, 출원인주소, 발명자, 발명자E, 발명자코드, 발명자주소, 발명자 우편번호, 발명자국적, 대표IPC, IPC코드, 요약, 미국특허분류, 대리인주소, 대리인코드, 대리인(한글), 대리인(영문), 국제공개일자, 국제공개번호, 국제출원일자, 국제출원번호, 우선권, 우선권주장일, 우선권국가, 우선권출원번호, 원출원일자, 원출원번호, 지정국, Citing Patents, Cited Patents
저장형식	Text(ASCII format) Excel format PIAS분석(.xls)
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Missile director 원문보기

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Missile director 원문보기

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