System and method to change SVS mode

    公开(公告)号:US11315434B2

    公开(公告)日:2022-04-26

    申请号:US16670788

    申请日:2019-10-31

    Abstract: A system may include a display and a processor communicatively coupled to the display. The processor may be configured to: output, to the display, a synthetic vision system (SVS) taxi mode exocentric view of an aircraft while the aircraft is performing taxi operations, while the aircraft is on ground, and when the aircraft is not in a predetermined exclusion zone, the predetermined exclusion zone including portions of a runway where the aircraft is able to begin taking off; and output, to the at least one display, an SVS flight mode egocentric view from the aircraft when the aircraft is in the predetermined exclusion zone. The display may be configured to display the SVS taxi mode exocentric view until the aircraft is in the predetermined exclusion zone and display the SVS flight mode egocentric view when the aircraft is in the predetermined exclusion zone.

    System for symbolically representing text-based obstacle data on an electronic map

    公开(公告)号:US10290216B1

    公开(公告)日:2019-05-14

    申请号:US15973732

    申请日:2018-05-08

    Abstract: Systems and methods for symbolically representing text-based obstacle data on an electronic map are disclosed. In embodiments, a system includes a receiver in communication with a remote server. The receiver is configured to receive one or more textual communications from the remote server. The system further includes an aircraft display system with a display and a controller. The controller is in communication with the display, the receiver, and a memory. The controller is configured to generate an electronic map at the display based on map data retrieved from the memory, wherein the map data includes geographic information and predetermined obstacle information. The controller is further configured to receive the one or more textual communications from the receiver and update the electronic map to include one or more symbolic representations based on obstacle data derived from the one or more textual communications.

    System and method for optimizing hold and divert operations

    公开(公告)号:US11156461B1

    公开(公告)日:2021-10-26

    申请号:US16400968

    申请日:2019-05-01

    Abstract: Systems and methods for providing decision support guidance are provided. A method includes receiving airport information that includes a location of each airport of a plurality of airports. The method further includes determining a flight range of an ownship based on a location of the ownship and an amount of fuel remaining in the ownship, and determining if any airport of the plurality of airports is within the flight range of the ownship. The method further includes, for each airport within the flight range: determining an amount of time the ownship can maintain a current flight course before the airport is no longer within the flight range; and providing display data. The display data indicates the amount of time the ownship can maintain the current flight course before the airport is no longer within the flight range.

    System and method for prevention and recovery from high altitude stalls

    公开(公告)号:US10723480B1

    公开(公告)日:2020-07-28

    申请号:US15799729

    申请日:2017-10-31

    Abstract: An aircraft-based stall prediction and recovery system may be embodied in a flight control system connected to aural/visual annunciators and flight controls (e.g., throttles and control surfaces). Based on received environmental data, the stall prediction and recovery system may detect imminent upset conditions (e.g., underspeed or overspeed) based on minimum and maximum operating speeds for the current airframe, altitude, and atmospheric conditions. The stall prediction and recovery system may notify the crew of the imminent upset and advise corrective measures. If a stall warning is received, the stall prediction and recovery system may engage an auto-recovery mode, notifying the crew of the engagement and restoring the aircraft to a safe target airspeed via automated recovery procedures, e.g., correcting the aircraft angle of attack and/or attitude. Upon resolution of the stall, the stall prediction and recovery system may disengage the auto-recovery mode, notifying the crew via the annunciators.

    System and Method to Change SVS Mode

    公开(公告)号:US20210358316A1

    公开(公告)日:2021-11-18

    申请号:US16675999

    申请日:2019-11-06

    Abstract: A system may include a display and a processor. The processor may: output a synthetic vision system (SVS) taxi mode exocentric view of an aircraft while the aircraft is performing taxi operations and when the aircraft is not in a predetermined exclusion zone, the predetermined exclusion zone including portions of a runway where the aircraft is able to begin taking off, wherein a width of the predetermined exclusion zone is based at least in part on at least one of a width of the runway or a classification of the runway; and output an SVS flight mode egocentric view from the aircraft when the aircraft is in the predetermined exclusion zone. The display may display the SVS taxi mode exocentric view until the aircraft is in the predetermined exclusion zone and display the SVS flight mode egocentric view when the aircraft is in the predetermined exclusion zone.

    Aircraft recording system, device, and method responsive to a new command not stated in a flight plan
    8.
    发明授权
    Aircraft recording system, device, and method responsive to a new command not stated in a flight plan 有权
    航空器记录系统,设备和方法,对飞行计划中没有说明的新命令做出回应

    公开(公告)号:US09534922B1

    公开(公告)日:2017-01-03

    申请号:US13625979

    申请日:2012-09-25

    CPC classification number: G01C23/00 G01C23/005

    Abstract: Present novel and non-trivial system, device, and method for recording a modification of an existing route plan are disclosed. The disclosed system may be comprised of a flight management system (“FMS”), at least one human-machine interface (“HMI”) device, at least one display unit, and a route modification generator (“RMG”). The disclosed device may be comprised of the RMG configured to perform the disclosed method, where such method may be comprised of receiving a request to modify an existing route plan; retrieving the route plan from the FMS; generating a message data set representative of one or more pre-formatted messages having one or more visually-conspicuous, user-interactive variable fields; updating the message data set in response to a user's selection of each field; sending the updated data set to the display unit; receiving a pilot's authorization to modify the route plan, and sending the accepted, modified flight plan to the FMS.

    Abstract translation: 公开了一种用于记录现有路线图的修改的新型和非平凡的系统,设备和方法。 所公开的系统可以包括飞行管理系统(“FMS”),至少一个人机接口(“HMI”)设备,至少一个显示单元和路由修改生成器(“RMG”)。 所公开的设备可以由被配置为执行所公开的方法的RMG组成,其中这种方法可以包括接收修改现有路线规划的请求; 从FMS检索路线图; 生成表示一个或多个预先格式化的消息的消息数据集,所述预格式化消息具有一个或多个视觉上显眼的,用户交互的可变字段; 响应于用户对每个字段的选择来更新消息数据集; 将更新的数据集发送到显示单元; 接收飞行员修改路线计划的授权,并将接受的修改的飞行计划发送给FMS。

    System and method to momentarily switch SVS mode

    公开(公告)号:US11097851B1

    公开(公告)日:2021-08-24

    申请号:US16687858

    申请日:2019-11-19

    Abstract: A system may include a display and a processor communicatively coupled to the display. The processor may be configured to: output, to the display, a synthetic vision system (SVS) taxi mode exocentric view of an aircraft when the aircraft is performing taxi operations and when the aircraft is on ground; receive a user input to switch the output of the SVS taxi mode exocentric view to an SVS flight mode egocentric view from the aircraft; and switch the output of the SVS taxi mode exocentric view to output, to the display, the SVS flight mode egocentric view when the aircraft is performing taxi operations and when the aircraft is on ground based at least on the user input to switch from the SVS taxi mode exocentric view to the SVS flight mode egocentric view.

    System and method for recovery from wake vortex encounters

    公开(公告)号:US10809743B1

    公开(公告)日:2020-10-20

    申请号:US15632072

    申请日:2017-06-23

    Abstract: An airborne platform includes an avionics controller circuit. The avionics controller circuit is configured to receive an ownship orientation from a sensor configured to detect the ownship orientation. The avionics controller circuit is configured to determine an orientation parameter based on the ownship orientation. The avionics controller circuit is configured to compare the orientation parameter to an orientation threshold. The avionics controller circuit is configured to determine the ownship to be in a wake vortex condition based on at least one wake vortex criteria, the at least one wake vortex criteria including the orientation parameter being greater than the orientation threshold for more than a predetermined period of time.

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