초록 ▼

A computationally efficient method for automatically generating lateral resolutions for air traffic control problems for a given aircraft allows for prediction and evaluation of required separation between aircraft, between aircraft and airspace, and problems with assigned metering time. Upon a poss

A computationally efficient method for automatically generating lateral resolutions for air traffic control problems for a given aircraft allows for prediction and evaluation of required separation between aircraft, between aircraft and airspace, and problems with assigned metering time. Upon a possible problem being predicted, lateral resolutions are created which provide plans to re-route the original flight trajectory of the aircraft in order to avoid a possible problem by examining the space surrounding the aircraft, iteratively adding data on each conflict encountered into a conflict database, calculating and probing maneuver trajectories for all conflicts in the conflict database, and selecting the most appropriate of the created maneuver trajectories.

대표청구항 ▼

A computationally efficient method for automatically generating lateral resolutions for air traffic control problems for a given aircraft allows for prediction and evaluation of required separation between aircraft, between aircraft and airspace, and problems with assigned metering time. Upon a poss

A computationally efficient method for automatically generating lateral resolutions for air traffic control problems for a given aircraft allows for prediction and evaluation of required separation between aircraft, between aircraft and airspace, and problems with assigned metering time. Upon a possible problem being predicted, lateral resolutions are created which provide plans to re-route the original flight trajectory of the aircraft in order to avoid a possible problem by examining the space surrounding the aircraft, iteratively adding data on each conflict encountered into a conflict database, calculating and probing maneuver trajectories for all conflicts in the conflict database, and selecting the most appropriate of the created maneuver trajectories. to the target gyration angle (φ*) from a predetermined linear characteristic, based on the target gyration angle (φ*), the gyration angle (φ), the gyration angular velocity (φ) and the gyration angular acceleration (φ), and determine the command value (u) to cause the control error (σ) to decrease. 9. A control device of a toroidal continuously variable transmission for a vehicle, the vehicle comprising an accelerator pedal, and the toroidal continuously variable transmission comprising an input disk, an output disk, a power roller which transmits torque between the input disk and the output disk, a trunnion which supports the power roller free to rotate, the trunnion comprising a trunnion shaft, the power roller varying a gyration angle (φ) according to a displacement (y) of the trunnion in the direction of the trunnion shaft to vary a speed ratio of the input disk and output disk, and an oil pressure actuator which drives the trunnion in the direction of the trunnion shaft, the device comprising: means for supplying oil pressure to the oil pressure actuator; means for connecting the trunnion and the control valve to feed back the displacement of the trunnion to the control valve; means for controlling the supplying means according to a command value (u); means for detecting a rotation speed (ωco) of the output disk; means for detecting a depression amount (APS) of the accelerator pedal; means for detecting the gyration angle (φ) of the power roller; means