IR jamming indicator for ATGM “Fagot”
- Solution against IR countermeasures
- Main features
- Ensures the possibility of reliable IR jamming discovery in wide band and narrow band field of view
- The indicator mass is 1.5 kg and it is easily mounted on the existing launching unit (significant improvement in relation to the original which weights 5 kg)
- Combat proven in Croatian Armed Forces, since 1996.
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Manual guidance unit for ATGM Fagot
- Solution against IR countermeasures
- Main features
- Digital control law implemented on the microcontroller
- Same mode of launching as in the semi-automatic mode of operation
- Easily mounted on the existing tripod
- No requirements for the external power supply
- Completely developed and manufactured
- Combat proven in Croatian Armed Forces, since 1996.
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Diagnostic station MDS-1 for ATGM "Fagot"
- Effective mean for testing, checking and adjusting parameters of the “Fagot” and “Konkurs” launchers and missiles.
- MDS-1 tests:
- Co linearity of optical and IR channels
- Angular amplification in channels
- Coordinate system rotation
- Electro-mechanical parts
- Position demodulator (X, Y amplification, offset, noise)
- Missile range unit (slope, linearity, slope discontinuity)
- Guidance control block (frequency response, compensation commands)
- Output command stage (reference waveform, command signal parameters)
- Launching control block
- Ignition unit
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Hardware in the loop (HIL) simulator for ATGM Fagot
- Special type of simulator designed for laboratory testing and validation experiments.
- Main features:
- Real time simulation of the 6DOF model of missile dynamics by using State-of-the-art DSP technology
- Real time simulation of missile and target kinematics
- Real optoelectronic sensor included in the simulation loop
- Digital guidance and control law
- Digital sensor signal processing
- Testing of the IR CCM algorithms.
- Completely developed and manufactured
- Several hundreds of “laboratory firings” have been performed
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Upgraded guidance unit for ATGM Fagot
- Old technology was replaced with new digital technology
- Digital guidance system was implemented
- Better maintainability and combat readiness
- Main features
- State-of-the-Art digital signal processors added
- Added digital signal processing algorithms for missile position computation
- New advanced IR CCM signal processing algorithms based on the blind signal separation theory were developed
- Improved accuracy of hitting moving targets due to the advanced guidance law
- Greater versatility, i.e. possibility of guiding several types of missiles with the same launcher
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