The invention relates to an airborne navigation
nacelle which is used for providing enemy destination parameters to a main
control room and comprises an inner ring platform, an outer ring frame and a base, wherein, the inner ring platform is hinged with the outer ring frame through a rotating shaft; the outer ring frame is hinged with the base through a hinge shaft; the base is fixed at the bottom of an
airplane; a visible light television imaging
system and a
laser rangefinder are arranged inside the inner ring platform; the inner ring platform comprises a two-degree-of-freedom
gyroscope, accelerometers, an imaging device, the
laser rangefinder and a double-channel rotary transforming angle
transducer; in addition, the outer ring frame comprises the double-channel rotary transforming angle
transducer; a micromachining
gyroscope is arranged on the base in the ordinate axis direction of an unmanned plane, measures the three-axis attitude of a carrier, and offsets the correlative navigation errors. Air speedometers are arranged in the ordinate axis direction and the
pitch axis direction of the unmanned plane; an
altimeter is arranged at the bottom of the base so as to measure the height of the unmanned plane; and the accelerometers are arranged at the two ends of the base so as to achieve
levelling when in initial alignment. The airborne navigation
nacelle can integrally detect, search and track a target, and has the advantages of high
system reliability and low cost.