No assignee for this patent application has been made.
Reporters obtained the following quote from the background information supplied by the inventors: "The subject matter described herein generally relates to flight planning for aircraft, and more specifically, to determining flight paths, speed, payload and fuel parameters that optimize one or more desired considerations (e.g., fuel, duration of travel) for an aircraft voyage.
"Flight planning has been important to air travel since before the advent of fixed-wing aircraft. Determining the range of an aircraft to deliver a given payload, the fuel required for such a trip, the bearings and altitudes to be used are all critical considerations for safe and efficient air travel.
"As fuel costs continue to rise and as concern about global climate change increases, a great amount of attention has been given in recent years to efficiency in air travel. Likewise, military applications look to efficiency, not only to minimize cost of operations but also to allow existing aircraft to transport greater payloads over longer distances. Efficiency also often translates into increased useful life for individual airframes and the ability to transport more cargo between aircraft overhauls.
"Central to many of these approaches is the recognition that an aircraft's range is based in part on its weight, which includes both the weight of the fuel it carries and of the static payload it is carrying. Recognition that a vehicle's payload capacity is related to the fuel it is carrying is not unique to aircraft; analysis of ships and land vehicles also recognizes the 'fuel as payload' issue. See, e.g., U.S. Pat. No. 5,880,408 (to assignee-at-issue
"Vehicular payloads are typically static over time, in that the weight of the payload does not vary from the beginning of a voyage to the end. Fuel is an aspect of payload that is virtually unique in that it varies dramatically in weight during the voyage.
"It has long been recognized that in aircraft, the varying weight of fuel is far too significant to be simply ignored, or even just averaged, in determining flight plans. Because fuel weight changes so dramatically over the course of a voyage, special computational techniques need to be used to account for the weight of fuel. In one simplistic approach, an iterative approach is used to gradually approach realistic estimation of flight characteristics such as range, endurance, and the like. Not only is such an approach inaccurate, it is computationally intensive and therefore either slow or expensive to use.
"Another approach is described in U.S. Pat. No. 6,134,500 (to assignee-at-issue
"Yet another approach to flight planning does not attempt to load enough fuel on the plane to clear all possible safety parameters for the journey from a worst-case perspective. Instead, a reasonably expected case is used for fuel loading calculations, and then divert locations are determined so that if conditions worse than expected arise, the aircraft can make an enroute determination to refuel using a 'reclear' procedure. Thus, far less fuel needs to be carried than for the conventional worst-case planning technique. However, more accurate and computationally simple mechanisms than the conventional ones for determining fuel loading are still applicable to such improved approaches to flight planning
"In military applications, another factor to be considered is the availability of in-flight refueling. Such refueling allows aircraft to take off with lighter fuel loads (and therefore heavier static payloads) than would normally be possible, or to take off in shorter distances than would be possible with full fuel tanks Determining where and how often to refuel to minimize cost can have dramatic impacts on overall mission costs.
"Commonly owned U.S. Pat. No. 8,010,242 addresses a number of these issues by including an initial, intentionally false assumption that the entire gross payload capacity of a plane is used for fuel. This assumption is used to seed an initial set of legal routes, after which an assumption is made that some fuel is removed, remaining legal routes are re-calculated, and so on until results are achieved that permit the desired amount of actual (i.e., non-fuel) payload to be placed on the aircraft.
"In spite of the long-understood need to consider fuel weight in flight planning, there remains a need for a computationally simple approach to help in determining factors such as flight path, fueling logistics and the like. Recently, the complexity of such planning has increased as additional parameters have been requested by aircraft operators. For instance, there is now interest in optimizing among fixed payload requirements, fuel requirements, ground track, altitude and speed. The first two factors are often selected initially as constraints, leaving the task as the optimum search within the four remaining dimensions. No quantitative methods exist that permit simple yet efficient determination of such factors."
In addition to obtaining background information on this patent application, VerticalNews editors also obtained the inventor's summary information for this patent application: "As disclosed herein, an optimization system is used that simplifies trip planning by route segments from a start point, the route segments collectively comprising a number of intermediate nodes; associating a multidimensional function relating to a first set of factors with each node; repeatedly choosing a subset of the segments responsive to the function and measure of acceptability at one or more of the nodes; expanding analysis to adjoining route segments by further selection responsive to the function and measure of acceptability, and selecting a preferred route based on the choosing and expanding.
"The features and advantages described in the specification are not all inclusive and, in particular, many additional features and advantages will be apparent to one of ordinary skill in the art in view of the drawings, specification, and claims. Moreover, it should be noted that the language used in the specification has been principally selected for readability and instructional purposes, and may not have been selected to delineate or circumscribe the inventive subject matter.
BRIEF DESCRIPTION OF DRAWINGS
"The disclosed embodiments have other advantages and features which will be more readily apparent from the following detailed description, when taken in conjunction with the accompanying drawings, in which:
"FIG. 1 is a flowchart indicating the high-level steps performed for flight planning, according to one embodiment.
"FIG. 2 is a high-level block diagram illustrating a computer system for implementing a preferred embodiment.
"FIG. 3 depicts potential legal routes for a particular flight from one location to another, showing exemplary issues to be considered in flight planning, according to one embodiment.
"FIG. 4 depicts an example graph of fuel usage as a function of duration of travel.
"FIG. 5 depicts modules for implementing a system according to one embodiment.
"FIG. 6 illustrates a method for selecting a route, according to one embodiment."
For more information, see this patent application: Ginsberg, Matthew L. Flight Planning System and Method Using Four-Dimensional Search. Filed
Keywords for this news article include: Patents, Airlines, Air Travel, Transportation.
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