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公开(公告)号：US12148311B2
公开(公告)日：2024-11-19
申请号：US17007822
申请日：2020-08-31
Applicant: Honeywell International Inc.
Inventor： Aralakuppe Yogesha , Shouvik Das , Mohammed Ibrahim Mohideen , Perumal Kumar , Rafeek Sainudeen , Parag Rao , Abhishek Alladi
Abstract: Disclosed are methods, systems, and non-transitory computer-readable medium for managing energy use in a vehicle. For instance, the method may include receiving forecasted data from a first external source, receiving real-time data corresponding to at least one weather parameter at a first location at a first time, and continuously determining whether to perform an adjustment to a control parameter of the vehicle by using a machine learning model that is based on the forecasted data for the at least one weather parameter, the real-time data for the at least one weather parameter, a battery condition of the vehicle, and/or an estimated amount of energy consumed by traveling along a first navigation path.
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公开(公告)号：US10894613B2
公开(公告)日：2021-01-19
申请号：US16208930
申请日：2018-12-04
Applicant: HONEYWELL INTERNATIONAL INC.
Inventor： Shouvik Das , Sunit Kumar Saxena , Rafeek Sainudeen , Naman Rawal
Abstract: Systems and methods for an auto-land system for a rotorcraft are provided. The system includes, a search light (SL) assembly configured to receive user input directing the SL to a point of interest (POI) and determine an actual SL orientation and an actual SL range to the POI; and, a searchlight controller operationally coupled to the search light assembly, and configured to: responsive to receiving a command to auto-land at the POI, begin (i) generating a desired trajectory from the rotorcraft actual orientation and rotorcraft actual range to the POI; (ii) generating guidance commands for navigating the rotorcraft in accordance with the desired trajectory; (iii) monitoring an actual SL range and an actual SL orientation; and (iv) generating controlling commands for the searchlight assembly in accordance with the coordinates of the POI.
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公开(公告)号：US20200172264A1
公开(公告)日：2020-06-04
申请号：US16208930
申请日：2018-12-04
Applicant: HONEYWELL INTERNATIONAL INC.
Inventor： Shouvik Das , Sunit Kumar Saxena , Rafeek Sainudeen , Naman Rawal
Abstract: Systems and methods for an auto-land system for a rotorcraft are provided. The system includes, a search light (SL) assembly configured to receive user input directing the SL to a point of interest (POI) and determine an actual SL orientation and an actual SL range to the POI; and, a searchlight controller operationally coupled to the search light assembly, and configured to: responsive to receiving a command to auto-land at the POI, begin (i) generating a desired trajectory from the rotorcraft actual orientation and rotorcraft actual range to the POI; (ii) generating guidance commands for navigating the rotorcraft in accordance with the desired trajectory; (iii) monitoring an actual SL range and an actual SL orientation; and (iv) generating controlling commands for the searchlight assembly in accordance with the coordinates of the POI.
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公开(公告)号：US08965671B2
公开(公告)日：2015-02-24
申请号：US13844804
申请日：2013-03-16
Applicant: Honeywell International Inc.
Inventor： Hardik Choksi , Rafeek Sainudeen , Nagaraj Sham
IPC: G08G5/06
CPC classification number: G08G5/065 , G08G5/0021
Abstract: An aircraft taxiing system is provided, comprising a flight control system, an electric taxi system having controls, a flight management system (FMS), at least one data input source coupled to the FMS, and a traffic collision avoidance system (TCAS). The FMS is programmed with instructions to calculate guidance speed and heading commands, augment the guidance commands to avoid runway incursions, and transmit the guidance commands to the flight control system. The TCAS is programmed with instructions to receive Automatic Dependent Surveillance-Broadcast (ADS-B) data from ground traffic, generate collision avoidance alerts; and transmit the collision avoidance alerts to the flight control system. The flight control system is programmed with instructions to receive guidance commands from the FMS, receive the traffic collision avoidance alerts from the TCAS, and compute the steering commands, and transmit the commands to the electric taxi system to taxi the aircraft along a calculated taxi route.
Abstract translation: 提供了一种飞行器滑行系统，包括飞行控制系统，具有控制的电动出租车系统，飞行管理系统（FMS），耦合到FMS的至少一个数据输入源以及交通防撞系统（TCAS）。 FMS用编程指令来计算引导速度和航向命令，增加引导命令以避免跑道入侵，并将指导命令传输到飞行控制系统。 TCAS编程具有从地面业务接收自动相关监控广播（ADS-B）数据的指令，产生避免碰撞警报; 并将防撞警报发送到飞行控制系统。 飞行控制系统被编程为具有从FMS接收指导命令的指令，从TCAS接收交通冲突避免警报，并计算转向命令，并将命令传送到电动出租车系统，以沿着计算的出租车路线 。
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