Patent Application
20220128354
Current radio altimeters are limited in range after which a “no computed data” value is set. This has resulted in several workarounds to determine when data is available and how it should be used at low altitudes. In addition to the limited technical capabilities of current altimeters, the FCC has approved repurposing of frequencies neighboring the C-band frequency which will degrade existing altimeter performance. Furthermore, traditional C-band altimeters require strong reflection from cement or asphalt to operate.
In one aspect, embodiments of the inventive concepts disclosed herein are directed to a radio altimeter with an electronically scanned array antenna. Orthogonal sweeps by the electronically scanned array antenna are used to identify a highest point in a region beneath the aircraft without the need for strong reflection.
In a further aspect, the electronically scanned array antenna is reconfigured to scan a subregion including the highest point with a higher frequency beam for a more accurate measurement.
In a further aspect, multiple sweeps are integrated over time for a more accurate measurement.
It is to be understood that both the foregoing general description and the following detailed description are exemplary and explanatory only and should not restrict the scope of the claims. The accompanying drawings, which are incorporated in and constitute a part of the specification, illustrate exemplary embodiments of the inventive concepts disclosed herein and together with the general description, serve to explain the principles.
The numerous advantages of the embodiments of the inventive concepts disclosed herein may be better understood by those skilled in the art by reference to the accompanying figures in which:
Before explaining at least one embodiment of the inventive concepts disclosed herein in detail, it is to be understood that the inventive concepts are not limited in their application to the details of construction and the arrangement of the components or steps or methodologies set forth in the following description or illustrated in the drawings. In the following detailed description of embodiments of the instant inventive concepts, numerous specific details are set forth in order to provide a more thorough understanding of the inventive concepts. However, it will be apparent to one of ordinary skill in the art having the benefit of the instant disclosure that the inventive concepts disclosed herein may be practiced without these specific details. In other instances, well-known features may not be described in detail to avoid unnecessarily complicating the instant disclosure. The inventive concepts disclosed herein are capable of other embodiments or of being practiced or carried out in various ways. Also, it is to be understood that the phraseology and terminology employed herein is for the purpose of description and should not be regarded as limiting.
As used herein a letter following a reference numeral is intended to reference an embodiment of the feature or element that may be similar, but not necessarily identical, to a previously described element or feature bearing the same reference numeral (e.g., 1, 1a, 1b). Such shorthand notations are used for purposes of convenience only, and should not be construed to limit the inventive concepts disclosed herein in any way unless expressly stated to the contrary.
Further, unless expressly stated to the contrary, “or” refers to an inclusive or and not to an exclusive or. For example, a condition A or B is satisfied by anyone of the following: A is true (or present) and B is false (or not present), A is false (or not present) and B is true (or present), and both A and B are true (or present).
In addition, use of the “a” or “an” are employed to describe elements and components of embodiments of the instant inventive concepts. This is done merely for convenience and to give a general sense of the inventive concepts, and “a” and “an” are intended to include one or at least one and the singular also includes the plural unless it is obvious that it is meant otherwise.
Finally, as used herein any reference to “one embodiment,” or “some embodiments” means that a particular element, feature, structure, or characteristic described in connection with the embodiment is included in at least one embodiment of the inventive concepts disclosed herein. The appearances of the phrase “in some embodiments” in various places in the specification are not necessarily all referring to the same embodiment, and embodiments of the inventive concepts disclosed may include one or more of the features expressly described or inherently present herein, or any combination of sub-combination of two or more such features, along with any other features which may not necessarily be expressly described or inherently present in the instant disclosure.
Broadly, embodiments of the inventive concepts disclosed herein are directed to a radio altimeter with an electronically scanned array antenna. Orthogonal sweeps by the electronically scanned array antenna are used to identify a highest point in a region beneath the aircraft without the need for strong reflection.
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In at least one embodiment, after identifying the highest point in the region, the processor 100 may configure the electronically scanned array antenna 104 to perform a second set of orthogonal sweeps of a subregion including the highest point. The second set of sweeps is configured to produce a more accurate altitude measurement. Such second sweep may also produce a more accurate location measurement of the highest point view a narrower beam angle.
In at least one embodiment, sweep return signals are stored in a data storage element 106 to be integrated over time. Such integration may produce increased location and altitude accuracy.
In at least one embodiment, the processor 100 operates the electronically scanned array antenna 104 as a pulse radar by iteratively, sequentially configuring the electronically scanned array antenna 104 to transmit and then receive. Furthermore, the electronically scanned array antenna 104 may be directed to reject sources of interference.
In at least one embodiment, radiating elements may be selectively disabled to significantly lower power usage for lower resolution sweeps. The electronically scanned array antenna 104 may be configured to operate in the X-band frequency. The electronically scanned array antenna 104 may be configured to produce cosecant squared beam pattern.
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In at least one embodiment, the electronically scanned array antenna may be configured to scan 506, 508 or sweep a subregion of the region below the aircraft at a higher resolution, the subregion including the highest point, along the axis from the tail-to-nose, and then along the axis from wingtip-to-wingtip. The altitude and position measurements may be refined 510 based on the return signals.
In at least one embodiment, sweep measurements may be stored over time and coherently integrated 512 to produce an accurate altitude map.
It is believed that the inventive concepts disclosed herein and many of their attendant advantages will be understood by the foregoing description of embodiments of the inventive concepts disclosed, and it will be apparent that various changes may be made in the form, construction, and arrangement of the components thereof without departing from the broad scope of the inventive concepts disclosed herein or without sacrificing all of their material advantages; and individual features from various embodiments may be combined to arrive at other embodiments. The form herein before described being merely an explanatory embodiment thereof, it is the intention of the following claims to encompass and include such changes. Furthermore, any of the features disclosed in relation to any of the individual embodiments may be incorporated into any other embodiment.
