RU2332634C1 - Method of functioning of information computation system of missile and device therefor - Google Patents
Method of functioning of information computation system of missile and device therefor Download PDFInfo
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- RU2332634C1 RU2332634C1 RU2007106616/02A RU2007106616A RU2332634C1 RU 2332634 C1 RU2332634 C1 RU 2332634C1 RU 2007106616/02 A RU2007106616/02 A RU 2007106616/02A RU 2007106616 A RU2007106616 A RU 2007106616A RU 2332634 C1 RU2332634 C1 RU 2332634C1
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Abstract
FIELD: missilery.
SUBSTANCE: invention is related to the field of aviation controlled missiles. Substance of invention consists in preparation of missile on board of carrier airplane for work, measurement of target movement parameters and missile own movement, generation of assessment of necessary parameters of target relative movement and missile absolute movement, selection of method of missile homing at target of the best application by any criterion for these conditions. Parameters of mismatch are calculated for selected method, the said parameters characterising extent of mismatch of actual parameters of missile movement and their required values. Analysis of jamming environment is carried out, noise protective facilities and non-radio-radar meters being switched on depending on jamming environment. Formation of preparation and control signal is carried out for radio proximity fuse. Based on current values, angle position and target range rate of missile approaching target is determined, as well as module of missile miss, geometric dimensions and target angle. On the basis of these data commands are generated for blasting of missile warhead and for initial speed of missile warhead fragments emission.
EFFECT: increased efficiency of operational use.
21 cl, 13 dwg
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Priority Applications (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
RU2007106616/02A RU2332634C1 (en) | 2007-02-21 | 2007-02-21 | Method of functioning of information computation system of missile and device therefor |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
RU2007106616/02A RU2332634C1 (en) | 2007-02-21 | 2007-02-21 | Method of functioning of information computation system of missile and device therefor |
Publications (1)
Publication Number | Publication Date |
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RU2332634C1 true RU2332634C1 (en) | 2008-08-27 |
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Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
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RU2007106616/02A RU2332634C1 (en) | 2007-02-21 | 2007-02-21 | Method of functioning of information computation system of missile and device therefor |
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RU (1) | RU2332634C1 (en) |
Cited By (2)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
RU2688717C1 (en) * | 2018-11-19 | 2019-05-22 | Акционерное общество "Научно-производственное предприятие "Дельта" | Autodyne radar fuse |
CN113959268A (en) * | 2021-10-20 | 2022-01-21 | 上海工程技术大学 | Rear-side missile cooperation method for intercepting and damaging hypersonic target along track |
-
2007
- 2007-02-21 RU RU2007106616/02A patent/RU2332634C1/en active
Cited By (3)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
RU2688717C1 (en) * | 2018-11-19 | 2019-05-22 | Акционерное общество "Научно-производственное предприятие "Дельта" | Autodyne radar fuse |
CN113959268A (en) * | 2021-10-20 | 2022-01-21 | 上海工程技术大学 | Rear-side missile cooperation method for intercepting and damaging hypersonic target along track |
CN113959268B (en) * | 2021-10-20 | 2023-03-10 | 上海工程技术大学 | Rear-lateral guidance combat matching method for front-track interception damage of hypersonic target |
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