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- It tends to increase the actual tracking errors in the system because the introduction of measurements from false alarms will have different noise properties to those of the target. - Secondly, the track could become ‘locked' onto the false alarm rather than the true target. Once several false alarms have been associated with the track, the track states reflect the properties of the false alarm rather than the target, making mis-association more likely. - This is the basis for many missile countermeasure systems (e.g. ?ares as EO countermeasures). - Since missiles can be programmed to ignore targets that undergo rapid manouveres (such as being dropped out of a flare/chaff dispenser), flares and radar decoys are now designed to follow the trajectory of the aircraft for a short distance to ‘lure' the missile away from the aircraft.
Source of drage Total Drag on an aerofoil is called profile drag - Skin friction • due to tangential force arising from friction - Pressure • Form - due to the inte
the nature and importance of the efficient market hypothesis and comment on the implications for managers and investors?
Flow Solver The flow solver of FP utilises data produced by the grid generator, together with data read from an input file named FLOW.DAT, and proceeds to calculate the solutio
explain the fibre optic communication system with block diagram
Shelf List Filing Shelf list reflects the arrangement of documents in the library. That is to say, the classificatory arrangement of the documents in a library can be seen th
dhpl is the firm situated in faridabad,its ending year on 31st march 2009 ,1000million asset base rs.650 million & the net profit of the company was 76 milloin the managmnt of the
Synchro resolvers for high load The receiver rotor is driven by an electric motor to a null position, i.e. the receiver coil will be aligned at 90 o to the transmitter coil. A
i want to make a project which is based on video transmission via laser ..please help me
I have senior design this semester and my professor give my this project. could you help me
Choked Nozzle Considering the formula for thrust under "choked" nozzle conditions: Thrust =(P-P 0 )A + WV j /g Where: P = Pressure P = Ambien
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