Embodiments provide systems, methods, and computer program products for optimizing cruise altitudes for multiple aircraft. The embodiments may be used for optimizing cruise altitudes of multiple aircraft on multiple flight paths and/or system capacity by an operator and/or an air navigation service provider. According to exemplary embodiments, a first set of optimum initial cruise altitudes are established for a plurality of aircraft. Weather conditions at the first set of optimum initial cruise altitudes are accounted for to establish a second set of optimum initial cruise altitudes. Direction of flight at the second set of optimum initial cruise altitudes is accounted for to establish a third set of optimum initial cruise altitudes. Any conflicts between aircraft at the third set of optimum initial cruise altitudes are detected. When a conflict is detected, the conflict is resolved to establish a fourth set of optimum initial cruise altitudes.
This information is part of a study by Oasis Global, Inc. of all space inventions filed at the United States Patent and Trademark Office, and is provided for informational purposes only. It is not an endorsement of any particular assignee, inventor or invention. Although Peter A. Koziol represents inventors and assignees of space inventions he does not represent all of the inventors and assignees listed. The prosecuting attorney agent or firm for each patent is identified by the United States Patent and Trademark Office in the patent specfication, which can be viewed by clicking on the patent image or downloading the patent document. For more information regarding Mr. Koziol's background and experience, or to learn more about space inventions, please contact Mr. Koziol.
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