A CONCEPTION FOR USING UNMANNED AIRCRAFT TO TECHNICAL CHECK FLIGHTS OVER MISSILE GUIDANCE STATION

Stanisław Grzywiński; Stanisław Żygadło; Maciej Podciechowski; Witold Baumgart

doi:10.5604/01.3001.0014.4879

A CONCEPTION FOR USING UNMANNED AIRCRAFT TO TECHNICAL CHECK FLIGHTS OVER MISSILE GUIDANCE STATION

PROBLEMY TECHNIKI UZBROJENIA ◽

10.5604/01.3001.0014.4879 ◽

2020 ◽

Vol 154 (2) ◽

pp. 7-20

Author(s):

Stanisław Grzywiński ◽

Stanisław Żygadło ◽

Maciej Podciechowski ◽

Witold Baumgart

Keyword(s):

Unmanned Aircraft ◽

Missile Guidance ◽

Missile System

The paper presents a conception for using an unmanned plane to technical check flights over the guidance station of NEWA S.C. antiaircraft missile system. The solution employs some adapted components of check flight instruments which are currently used and some newly developed units.

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GPS Inertial Missile Guidance System

Pakistan Journal of Engineering Technology & Science ◽

10.22555/pjets.v4i2.207 ◽

2015 ◽

Vol 4 (2) ◽

Author(s):

Osama Sarfaraz

Keyword(s):

Target Position ◽

Guidance System ◽

Missile Guidance ◽

Radio Waves ◽

Current Position ◽

Google Maps ◽

Main Component ◽

Missile System

The task of this work is to design the guidance system for the missile which would guide the missile accurately to hit the target as directed. Guidance is the main component of the missile system which helps in hitting the target accurately. The missile can be guided by the number of ways which includes by using laser, GPS infrared or radio waves on its way to the target. This paper proposes a model to guide the missile with the help of GPS and INS. This model requires a computer or controller which should be installed in the missile to control the missile flight according to the guidance provided by GPS and INS. The system works by knowing the missile current position and the position of the target. The position of the target is known by using Google maps which is feed in the missile controller before the missile is launched. Missile current position is known by using GPS while the missile current orientation and heading is known by using INS. Missile current position is compared with the target position to calculate the desired heading towards the target, then missile controller auto pilots the missile according to the desired heading towards target to hit the target.

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Research on Missile System with Strapdown Guidance Technology

Advanced Materials Research ◽

10.4028/www.scientific.net/amr.785-786.1560 ◽

2013 ◽

Vol 785-786 ◽

pp. 1560-1563

Author(s):

De Long Feng ◽

Suo Chang Yang ◽

Ying Xi Liu

Keyword(s):

Inertial Measurement Unit ◽

Simulation Experiment ◽

Low Cost ◽

Guidance System ◽

Measurement Unit ◽

Missile Guidance ◽

Inertial Measurement ◽

Guidance And Control ◽

And Control ◽

Missile System

This paper presents a project of missile guidance system based on the strapdown guidance technology. The project is composed of strapdown seeker and inertial measurement unit. The integrated guidance and control technology have been adopted. The project raise accuracy of missiles on the premise that the low cost should be guaranteed. According to simulation experiment, this paper proves the feasiblity of the scheme, and it has good ballistic missile.

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INDICATORS OF SA-19 “GRISON” ANTI-AIRCRAFT GUN MISSILE SYSTEM EFFICIENCY WHEN FIRING AT NONTYPICAL TARGETS OF THE ROCKET AND ARTILLERY WEAPONS

Наукові праці Державного науково-дослідного інституту випробувань і сертифікації озброєння та військової техніки ◽

10.37701/dndivsovt.9.2021.12 ◽

2021 ◽

pp. 88-96

Author(s):

D. Lytovchenko ◽

V. Kutsenko

Keyword(s):

Missile Guidance ◽

System Efficiency ◽

Conditional Probabilities ◽

Slant Range ◽

Single Target ◽

Small Targets ◽

Use Factors ◽

Missile System

In modern conditions of combat use the SA-19 “Grison” anti-aircraft gun missile system fires at small targets (drones) and typical targets (helicopters and attack aircraft), so a number of problems arise. In particular, they include: finding the value of the probabilities of hitting the target with n shots and one shot; assessing the effectiveness of the SA-19 “Grison” platoon‟s concentrated fire on a single target; estimating errors of missile guidance and warhead detonation system; estimating the values of conditional probabilities of hitting a target with a single missile, depending on the value of particular mishit. When calculating the slant range to the far edge of the SA-19 “Grison” weapon's kill zone under different conditions of use, factors that reduce these ranges should be taken into account. An analysis of the main studies and publications presented in [1-9] does not make it possible to determine the performance of missile and artillery weapons in shooting at small-size targets. This literature provides general approaches to solving this problem. The purpose of this article is to develop a model for calculating the values of conditional probabilities of destruction of small targets, to form the best options for repelling an enemy‟s air strike, as well as to justify the general directions of improvement of weapon‟s elements.

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