摘要:
The present invention provides several apparatus, methods, and computer program products for generating a terrain clearance floor envelope for use in a ground proximity warning system. In one embodiment, the present invention includes a processor that defines a terrain clearance floor envelope having at least two boundaries. In this embodiment, the processor defines at least one of the boundaries based on a runway position quality factor, an altitude data quality factor, and an aircraft position quality factor. Using these factors, the processor of the present invention can more precisely define the boundaries of the envelope about the selected runway. Further, the processor of the present invention does not unnecessarily increase the region between the envelope and runway where no ground proximity alarms are generated. In another embodiment, the present invention includes a processor that defines the terrain clearance floor envelope to be asymmetrical, such that respective profiles of the envelope in a radial cross-section are different in at least two radial directions from a center point of the selected runway. Importantly, in one embodiment of the present invention, the processor defines end regions of the terrain clearance floor envelope adjacent to the ends of the selected runway to have a different slope profile than side regions of the terrain clearance floor envelope adjacent to the sides of the selected runway. This, in turn, allows the processor to define the end regions to reflect a landing pattern for an aircraft approaching the end of the selected runway, while also defining the side regions to reflect a flight pattern for an aircraft approaching the side of the selected runway.
摘要:
In a solid-state image device comprising an image storage block having a block surface, a plurality of storage elements are embeded along the block surface to store an image in the form of electric charge. An overlying layer is deposited to form an array of optical lenses in correspondence to the storage elements. An intermediate layer is laid between the block surface and the overlying layer. Incident light focuses through the lenses and the intermediate layer onto the storage elements. The intermediate layer serves as an adjusting layer for adjusting a focal length.
摘要:
A solid-state imaging device has a semiconductor substrate of one conductive type. A plurality of light-charge converter regions, of the opposite conductivity type, are formed in the semiconductor substrate. A charge-voltage converter region, formed in the semiconductor substrate, converts the electric charge produced by the light-charge converter regions into a voltage. At least one charge transfer section is formed in the semiconductor substrate for transferring the electric charge produced by the light-charge converter regions to the charge-voltage converter region. At least one charge transfer gate section is in the semiconductor substrate and has a gate electrode for controlling the timing of a transfer of the electric charges from the light-charge converter regions to the charge transfer section. Pulses are generated with a predetermined pulse potential and applied to the gate electrode in the charge transfer gate section. The predetermined pulse potential has the relationshipV.sub.B +2.phi..sub.FP
摘要:
A two-dimensional charge-coupled device for relatively high resolution image pick up includes an imaging area, a storage area, and plural output registers for developing plural video signals delayed by predetermined intervals, e.g., integral multiples of one horizontal line trace period. The several register output signals are combined to provide a composite video signal characterized by a greater resolution vis-a-vis the direct CCD output.
摘要:
Systems and methods for adjusting target approach speed for use in a “Too Fast” approach to landing condition. An exemplary system stores predefined maximum wind setting and a predefined reference speed and a pilot set bug speed value. A processing device sets a target speed equal to the bug speed, if the bug speed is less than the reference speed plus a value associated with a predefined maximum wind setting, and sets the target speed equal to the reference speed plus the max wind added value, if the manual bug speed is not less than the reference speed plus the max wind added value. An output device outputs an alert if the received aircraft speed is greater than the set target speed plus a predefined error value when the received aircraft location is within a threshold value of a touchdown point.
摘要:
Systems and methods to provide alerts when a rotorcraft is in a low airspeed condition. During takeoff or go-around, an aural alert is provided to the pilot before the aircraft slows to less than the effective translational lift speed. The aural, visual, and/or tactile alert gets the pilot's attention to manage the aircraft's airspeed before it is too late in this critical flight phase.
摘要:
Systems and methods that alert the pilot of the unusual negative pitch attitude. Additionally, the system can bias a “sink rate” envelope toward a more sensitive direction, such that the pilot can be alerted while (or before) a large sink rate is built up during an unusual negative pitch attitude condition.
摘要:
Systems and methods for monitoring Required Navigational Performance (RNP) Procedures and reducing nuisance Enhanced Ground Proximity Warning System warnings including a processor, a memory with RNP instructions and data, and a communication device. The processor accesses the RNP data and instructions from the memory, and uses the communication device to obtain flight information from a Flight Management System of an aircraft. When the processor determines that the aircraft is in RNP space, the processor projects an RNP envelope and modifies a warning envelope of an EGPWS to coincide with the RNP envelope if the EGPWS warning envelope extends farther than the RNP envelope.
摘要:
Systems, methods and computer program products for alerting a flight crew during landing that the tailwind exceeds acceptable limits. The system determines a base tailwind threshold speed for a candidate runway based on a performance constant associated with an aircraft and candidate runway information and determines present tailwind speed. If the tailwind speed is greater than the base tailwind threshold speed, a tailwind alert is generated. Also, the system determines if the aircraft is in a tailwind alerting mode based on configuration of the aircraft and activates tailwind alerting, if it is determined that the aircraft is in the tailwind alerting mode.