JPS6451505A - Initiation signal generator - Google Patents

Initiation signal generator

Info

Publication number
JPS6451505A
JPS6451505A JP62207492A JP20749287A JPS6451505A JP S6451505 A JPS6451505 A JP S6451505A JP 62207492 A JP62207492 A JP 62207492A JP 20749287 A JP20749287 A JP 20749287A JP S6451505 A JPS6451505 A JP S6451505A
Authority
JP
Japan
Prior art keywords
initiation signal
beams
antenna
relative speed
vehicle
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.)
Pending
Application number
JP62207492A
Other languages
Japanese (ja)
Inventor
Kiyoshi Nakahara
Hideo Fukuda
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
Mitsubishi Electric Corp
Original Assignee
Mitsubishi Electric Corp
Priority date (The priority date 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 date listed.)
Filing date
Publication date
Application filed by Mitsubishi Electric Corp filed Critical Mitsubishi Electric Corp
Priority to JP62207492A priority Critical patent/JPS6451505A/en
Publication of JPS6451505A publication Critical patent/JPS6451505A/en
Pending legal-status Critical Current

Links

Landscapes

  • Control Of Position, Course, Altitude, Or Attitude Of Moving Bodies (AREA)
  • Selective Calling Equipment (AREA)

Abstract

PURPOSE:To generate the initiation signal of a warhead at an optimum period and to securely destroy a target vehicle by controlling the direction of the beams of an antenna in correspondence with a relative speed between flying vehicle and the target plane. CONSTITUTION:A beam direction controller 9 decides the phase-shifting quantity of a phase shifter 10 based on the relative speed 8 when the flying vehicle 2 passes through the side of the target plane 1. The phase shifter 10 steers the beams of the antenna 3 in accordance with the phase-shifting quantity. If the relative speed is fast, the beams of the antenna steer farther like B2. If the relative seed is slow, the beams of the antenna steer more backward like B3. Since the relation of positions of the flying vehicle 2 and the target plane 1 when the initiation signal 6 is generated can be changed thus, the initiation signal is generated at the optimum period even at any relative speed and the target vehicle can securely be destroyed.
JP62207492A 1987-08-21 1987-08-21 Initiation signal generator Pending JPS6451505A (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
JP62207492A JPS6451505A (en) 1987-08-21 1987-08-21 Initiation signal generator

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
JP62207492A JPS6451505A (en) 1987-08-21 1987-08-21 Initiation signal generator

Publications (1)

Publication Number Publication Date
JPS6451505A true JPS6451505A (en) 1989-02-27

Family

ID=16540622

Family Applications (1)

Application Number Title Priority Date Filing Date
JP62207492A Pending JPS6451505A (en) 1987-08-21 1987-08-21 Initiation signal generator

Country Status (1)

Country Link
JP (1) JPS6451505A (en)

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN103576689A (en) * 2013-10-08 2014-02-12 北京控制工程研究所 Rendezvous and docking six-degree-of-freedom relative control method

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN103576689A (en) * 2013-10-08 2014-02-12 北京控制工程研究所 Rendezvous and docking six-degree-of-freedom relative control method

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