초록 ▼

There is provided a guidance system for allowing an air vehicle to guide a moving object, comprising a Synthetic Aperture Radar located on the air vehicle, and a means of communication for allowing the air vehicle to communicate with the moving object, wherein the Synthetic Aperture Radar is capable

There is provided a guidance system for allowing an air vehicle to guide a moving object, comprising a Synthetic Aperture Radar located on the air vehicle, and a means of communication for allowing the air vehicle to communicate with the moving object, wherein the Synthetic Aperture Radar is capable of determining the position and orientation of the air vehicle relative to a desired location, and information provided by the Synthetic Aperture Radar is used, via the means of communication, to guide the moving object towards the desired location. A guidance system wherein a seeker is utilised on the moving object is also provided. The invention further provides a method for allowing an air vehicle to guide a moving object towards a desired location comprising the steps of using a Synthetic Aperture Radar to determine the position and/or orientation of the air vehicle relative to a desired location, establishing a communications link for allowing the air vehicle to communicate with the moving object, using the communications link to provide information to the moving object and thereby to guide the moving object towards the desired location. A method wherein a seeker located on the moving object is utilised is also provided. The invention further provides methods for aligning a radar beam with a target in a Synthetic Aperture Radar image.

대표청구항 ▼

The invention claimed is: 1. A guidance system for allowing an air vehicle to guide a moving object, comprising a synthetic aperture radar, located on the air vehicle, for determining a position of said air vehicle relative to a desired location; a steerable radar information field generated by sai

The invention claimed is: 1. A guidance system for allowing an air vehicle to guide a moving object, comprising a synthetic aperture radar, located on the air vehicle, for determining a position of said air vehicle relative to a desired location; a steerable radar information field generated by said radar and directed towards said moving object, said moving object located within said radar information field; and a receiver, located on said moving object, for receiving said radar information field and determining a relative position of said moving object within said radar information field, wherein the moving object maintains a constant position relative to said radar information field and, by said air vehicle steering said radar information field, the moving object is guided towards the desired location. 2. A guidance system as claimed in claim 1 wherein the means of communication comprises a command link for transmitting guidance data to the moving object. 3. A method for allowing an air vehicle to guide a moving object towards a desired location comprising the steps of: determining the position of the air vehicle relative to a desired location using a synthetic aperture radar located on said air vehicle, using said radar to generate a steerable radar information field; directing said radar information field towards said moving object so as to locate said object within said radar information field; locating a receiver on said moving object for receiving said radar information field and determining a relative position of the moving object within said radar information field; adjusting the relative position of the moving object within the radar information field by steering the moving object towards a predetermined relative position within the radar information field; and steering the radar information field towards said desired location while ensuring the moving object remains within said radar information field, thereby guiding the moving object towards the desired location. 4. A method as claimed in claim 3 wherein the synthetic aperture radar is used intermittently. 5. A method as claimed in claim 3 comprising the step of determining the angular relationship between the synthetic aperture radar and the radar information field. 6. A method as claimed in claim 3 wherein the radar information field is provided intermittently. 7. A method as claimed claim 3 wherein the moving object is launched such that its trajectory allows the moving object to encounter the radar information field. 8. A method as claimed in claim 3 further comprising the steps of tracking the moving object, then steering a radar information field onto the moving object and subsequently using the radar information field to steer the moving object towards the desired location. 9. A method as claimed in claim 3 wherein the radar information field is used to guide the moving object along part of its course and an inertial navigation system located on the moving object is used to guide the moving object along another part of its course. 10. A method for aligning a synthetic aperture radar beam with a target in a synthetic aperture radar image, said method comprising the steps of: forming sum and difference beams using said radar, steering the radar beam in pitch and yaw so that returns at the target range and Doppler shift are on the radar boresight and are therefore nulled out in the difference patterns, and calculating the direction of the target using the pitch and yaw angles through which the beam has been steered. 11. A method for aligning a synthetic aperture radar beam with a target in a synthetic aperture radar image, said method comprising the steps of: generating the radar beam using a phased array radar antenna having several elements, forming a space-time covariance matrix of the elements' outputs from the received return data, subjecting the covariance matrix to spatial-temporal spectral analysis, and determining the angle of the target with respect to the array using spectral analysis. 12. A method for aligning a radar beam with a target in a Synthetic Aperture Radar image comprising the steps of using a phased array radar for generating a Radar Information Field, the Radar Information Field being generated by at least two different Radar Information Field transmit beams, the different transmit beams each being offset from the radar boresight in different directions, using the same receive beam for receiving target return signals from all the transmit beans, integrating the target return signals from each of the different transmit beams separately, adding together the integrated target return signals to form a composite Synthetic Aperture Radar image, and using the relative amplitudes of the target return signals of the different transmit beams to provide target angular measurement.