摘要:
A method of creating a highly directional acoustic beam that can be swept er the water near the entrance of a harbor or channel location. The information provided to a boat operator as a result of the acoustic beam includes the operator's absolute bearing from the acoustic source. The nonlinear acoustic beam has a narrow beamwidth and is produced by small transducers that can be rotated in a selected scanning motion to provide a sequence of acoustic signals easily recognizable by the unaided human air of the boat operator who is cognizant of the acoustic sequence.
摘要:
An antenna and scanning means therefor particularly useful in an aircraft landing system operating in the microwave frequency range. The antenna is of the line phased array type which includes digitally controlled phase shifters for each of the radiating elements of the array. The beam formed by the antenna is steered by incrementing the phase shift applied at each of the array radiating elements by an amount of phase which is dependent in part upon the position of the radiating element in the array. Phase increments sufficient to shift the beam position by one coarse step (0.1.degree.) are applied to symmetrically located radiating element pairs, pair by pair, until all elements have been incremented. The beam is thereby caused to move through one coarse step in a number of fine steps equaling the number of pairs of elements in the array. An additional feature of the scanning means is the application of phase increment to the array elements in a pseudo-random sequence.
摘要:
An aircraft instrument landing system is disclosed wherein elevation angle measurements of an aircraft are derived by providing, in such system, a means for inhibiting an elevation swept beam of radiation from sweeping through ''''low'''' angles where significant multipath transmission is expected. Means are provided to vary the power in the transmitted beam of radiation in a predetermined manner as the beam is inhibited from sweeping. As a result the radiation received by the low flying aircraft is shaped in a way related to the shape of the received radiation expected without multipath transmission. Such arrangement enables the same aircraft receiver and processor to determine the elevation angles of both ''''high'''' and low flying aircraft without appreciable error.