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Consequently, one expects a certain amount of degradation in accuracy between bombing range results and operational results with this type of bombing system. It becomes unnecessary to know target altitude with a radar altimeter since this measures altitude above terrain directly. Given that the pursuer is not usually situated directly above the target at the instant of release, the flatness of the tcrrain between the release point and the target to a large extent determines the bombing accuracy associated with a radar altimeter.

FCS. The function of the FCS is to control the pursucr in pitch, yaw, and roll motion. The FCS executes the guidance commands and stabilizes the pursuer in flight. The FCS, upon receiving commands from the guidance law, then issues its own commands to the appropriate aerodynamic andlor thrust controls of the pursuer so that the guidance command can be properly executed. It is usually configured as a system equipped with low-accuracy inertial components (gyros and accelerometers). Small tactical missiles and most large transport vehicles often have open-loop control instead of the more complex FCS control.

When, however, the problem is that of conducting a precise system analysis, then a specific dynamic model is assumed for a particular seeker, and this is integrated with that o f the pursuer. Three homing configurations are assumed: passive, active, and semiactive. In the passive case, only the LOS angle is available through an 1R seeker. In the active homing case, both range and closing-velocity radar information are available through measurements, but in the semiactive mode, these measurements are bistatic.

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Aircraft powerplant handbook

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