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By Goeder F. P.

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For aircraft nose cone radar, antenna size is limited. You can find a compromise solution around X-band (λ = 3 cm). For missile seekers, the antenna size is even smaller and should be in Ku-band (compatible with shorter range). Finally, should you need to increase frequency for specific applications (missiles, detection of power lines), you should choose transmission windows (34 GHz, 94 GHz), located between the absorption lines of the atmospheric components. Note: This absorption is taken into account in the radar equation by the microwave loss term l (see Chapter 3).

Moreover, the carrier weapons system itself forms part of a wider /DFRPPH5DGDUERRN 3DJH  0RQGD\ )HEUXDU\    30 18 Part I — General Principles operational system and therefore needs to communicate with this larger system and “act” coherently with it. Despite its complexity and importance within the weapons system, radar is only a part of the system. It can therefore only be designed in relation to the missions, carriers, weapons, specific functions, and performance requirements. 2.

The angular difference measurement is given by the following equation: ∆ Σ⋅∆ ---------- Σ ( * $ ( α )6 ± * % ( α )6 ) ( * $ ( α )6 * % ( α )6 ) --------------------------------------------------------------------------------------------------- * $ ( α )6 * % ( α )6 *$ ( α ) ± *% ( α ) -------------------------------------* $ ( α ) *% ( α ) This equation is based exclusively on the direction of arrival, α (angular difference with respect to the axis), and the patterns GA(α) and GB(α). It is known as amplitude monopulse.

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