|국가/구분||United States(US) Patent 등록|
|미국특허분류(USC)||701/014; 701/003; 701/010; 244/001N; 702/039|
|발명자 / 주소|
|출원인 / 주소|
|대리인 / 주소||
|인용정보||피인용 횟수 : 2 인용 특허 : 8|
The present invention is an improved real-time, interactive sonic boom display for aircraft. By using physical properties obtained via various sensors and databases, the invention determines, in real-time, sonic boom impacts locations and intensities for aircraft traveling at supersonic speeds. The information is provided to a pilot via a display that lists a selectable set of maneuvers available to the pilot to mitigate sonic boom issues. Upon selection of a maneuver, the information as to the result of the maneuver is displayed and the pilot may procee...
1. An improved real-time, interactive sonic boom display for an aircraft, comprising: a processor configured to calculate a sonic boom near field source based on aircraft flight parameters, ray tracing the sonic boom to a ground location based on the sonic boom near field source, terrain data, aircraft information, and environmental condition data, signature aging the sonic boom due to nonlinear effects based on the ray tracing, and calculating a boom footprint and Mach cutoff condition based on the signature aging and ray tracing;a library file to provi...