Abstract: A method is provided for inferring the aircraft intent of an aircraft from an observed trajectory. Aircraft performance data relating to that type of aircraft is retrieved from memory, along with atmospheric conditions along the observed trajectory. An initial set of candidate aircraft intents is generated. Each aircraft intent provides an unambiguous description of how the aircraft may be flown that allows a determination of an unambiguous resulting trajectory. A computer system calculates a trajectory defined by each candidate aircraft intent and forms a cost function from a comparison of each calculated trajectory to the observed trajectory. An evolutionary algorithm evolves the initial candidate aircraft intents, wherein the evolutionary algorithm uses a multi-objective cost function to obtain a cost function value that measures the suitability of each candidate aircraft intent.

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: This disclosure is concerned with a method of detecting conflicts between aircraft passing through managed airspace, and to resolving the detected conflicts strategically. The method may include obtaining intended trajectories of aircraft through the airspace, detecting conflicts in the intended trajectories, forming a set of the conflicted aircraft, calculating one or more revised trajectories for the conflicted aircraft such that the conflicts are resolved, and advising the conflicted aircraft subject to revised trajectories of the revised trajectories.

Abstract: Systems and methods are operable maintain a proscribed Self Separation distance between an unmanned aircraft system (UAS) and an object. In an example system, consecutive intruder aircraft locations relative to corresponding locations of a self aircraft are determined, wherein the determining is based on current velocities of the intruder aircraft and the self aircraft, and wherein the determining is based on current flight paths of the intruder aircraft and the self aircraft. At least one evasive maneuver for the self aircraft is computed using a processing system based on the determined consecutive intruder aircraft locations relative to the corresponding locations of the self aircraft.

Abstract: Disclosed are algorithms and agent-based structures for a system and technique for analyzing and managing the airspace. The technique includes managing bulk properties of large numbers of heterogeneous multidimensional aircraft trajectories in an airspace, for the purpose of maintaining or increasing system safety, and to identify possible phase transition structures to predict when an airspace will approach the limits of its capacity. The paths of the multidimensional aircraft trajectories are continuously recalculated in the presence of changing conditions (traffic, exclusionary airspace, weather, for example) while optimizing performance measures and performing trajectory conflict detection and resolution. Such trajectories are represented as extended objects endowed with pseudo-potential, maintaining objectives for time, acceleration limits, and fuel-efficient paths by bending just enough to accommodate separation.

Abstract: An aerological phenomena alert device for an aircraft, which comprises onboard equipment capable of detecting meteorological phenomena, comprises: a module for collecting and storing meteorological data originating from the onboard equipment capable of detecting the meteorological phenomena, a module for creating a report from the collected meteorological data, a module for sending the report, a module for receiving reports sent by surrounding aircraft, a module for processing and consolidating the reports received, and for generating alerts when a report signals an aerological phenomenon, and a module for merging the data originating from aircraft and from meteorological stations, situated in a station on the ground and comprising a ground/air communication module for sending meteorological reports adapted to each aircraft according to its position in relation to an aerological phenomenon.

Abstract: An operational reliability system includes a flight grouping module, a block modification module, and a pairing optimizer. The system evaluates potential modifications to scheduled flight block time and quantifies associated changes in on-time performance B0. The system also evaluates the impact of block modifications to headcount, regulatory compliance, operating expenses, and so forth. Via use of the operational reliability system, compliance with external regulations, for example Federal Aviation Regulations (FAR), may be achieved with a higher degree of probability.

Abstract: An alerts and procedures management system for an aircraft comprises a software kernel aboard the aircraft and a parameterization tool for the software kernel, which comprises a conversion module for converting a configuration file describing an operational need of the system into a database of binary parameters which is able to parameterize the software kernel. The software kernel comprises at least four elementary cells: a first cell for acquiring aircraft signals, a second cell for characterizing state variables of the aircraft, a third cell for computing at least one separate event, a fourth cell for scheduling the separate events for communication with the crew; each of the cells comprising a software engine parameterizable by the database.

Abstract: An avionic system including: a memory that stores a selectable hash table assigned to a flight plan of an aircraft fleet, the hash table including table elements with operational parameters of an airport, wherein airports covered by the table elements are airports flown to according the fight plan of the aircraft fleet; and a plurality of ground stations situated at the flown to airports of the fight plan, wherein the ground stations are linked via a communication network to a central processing unit; a receiver of the central processing unit that receives, via a communication network interface, a transmission from a detection device, the transmission including at least parameters regarding a time interval parameter of an airport closing and an airport identification.

Abstract: Methods and system are provided for scheduling and negotiating air traffic within an airspace surrounding an airport and scheduled to land at the airport. An air traffic control (ATC) system is used to monitor the altitudes, speeds and lateral routes of aircraft. The ATC system generates a scheduled time-of-arrival (STA) at one or more meter fix points associated with the airport, the STA is stored, and data is received or inferred with the ATC system for at least a first of the aircraft, including a minimum fuel-cost speed and predicted trajectory parameters of the first aircraft based on current values of its existing trajectory parameters. Auxiliary data, including earliest and latest estimated time-of-arrival (ETAmin) and (ETAmax) at the meter fix point, STA being within/ outside ETAmin, ETAmax are generated, instructions are transmitted to the first aircraft, and the STA is updated for each aircraft stored in a queue.

Abstract: Method for identifying an airplane in connection to parking of the airplane at a gate or a stand, for possible connection of a passenger bridge (1) or a loading bridge to a door of an airplane, where the airplane is positioned and stopped at a predetermined position using a touchless measurement of the distance between the airplane and a fixed point, where the distance is indicated on a display (6) mounted in front of the pilot of the airplane on for instance an airport building (7), which display (6) shows the position of the airplane (5) in relation to a stop point for the airplane and shows the current airplane type, where the distance measurement and display are caused to be activated by a computer system (20) belonging to the airport or manually, and wherein an antenna (16) is caused to receive information (17) transmitted by an airplane.

Abstract: A handle bar route extension mechanism for creating or modifying a flight route. The handle bar route extension mechanism can allow a user to create or modify a flight route using a destination point. The handle bar route extension mechanism can be automatically rendered in a display in response to a touch input. In some configurations, the handle bar route extension mechanism may be rendered in a display in various directions or various lengths based on different inputs. In further configurations, more than one handle bar route extension mechanism may be rendered in a display.

Abstract: A method for constructing a flight trajectory of an aircraft, comprises a step of computing a sequence of state vectors (Ei) representing the trajectory of the aircraft; a state vector (Ei+1) being determined on the basis of the state vector (Ei) preceding it by means of: a step of computing the speed components (Vi+1), consisting in determining: a flight setpoint, by selecting an objective navigation point, a joining strategy adapted to the flight setpoint and to the flight domain (DV) by means of a predefined library (LSr) of joining strategies, a manoeuvre by means of the flight domain (DV), making it possible to follow the joining strategy towards the flight setpoint; a step of computing the other components of the state vector (Ei+1), on the basis of the components of the speed vector (Vi+1) and of the preceding state vector (Ei).

Abstract: According to aspects of the embodiments, there is provided an apparatus and method to synchronize trajectories from independent systems such as from a flight management system and the ground Air traffic control during the entire history of a flight. Since a number of trajectory discrepancy factors will intervene during the lifetime of a flight, such as a change in flight intent, controller intervention, or large deviations of the actual flight from the predicted trajectory due to prediction errors, there is need to dynamically monitor these deviations and control a dynamic synchronization cycle. A dynamic trajectory synchronization algorithm attempts to bring each of the systems back into balance whenever a disturbance causes an imbalance.

Abstract: Methods and apparatus for enabling an air traffic control system to set a beacon code on a transponder of an aircraft without voice communication with the flight crew. In one embodiment, an air traffic control system receives a flight plan from an aircraft, relays clearance of the flight plan to the aircraft, sets a beacon code on a transponder on the aircraft without voice communication, receives an acknowledgement of the beacon code setting from the aircraft, sends an acknowledgement to the aircraft, sets a new beacon code on the transponder without voice communication and receives a new acknowledgement of the new beacon code from the aircraft.

Abstract: A system for controlling an image displayed on a display unit of an aircraft is shown and described. The system includes an enhanced vision system that detects elements of an approach lighting system for display on the display unit. The system also includes a synthetic vision system that uses a database of navigation information and a determined aircraft location to generate synthetic display elements representing the approach lighting system. Display electronics of the system cause the detected elements from the enhanced vision system to be simultaneously displayed on the display unit within a same scene as the generated synthetic display elements from the synthetic vision system. Advantageously, the simultaneous display allows a pilot viewing the display unit to check for whether information provided by the enhanced vision system matches information provided by the synthetic vision system.

Abstract: An electronic flight planning system is provided, arranged to implement a preferred method for identifying conflicts between flight plans for aircraft. In the preferred method, the system receives, as data input from one or more users, a plurality of flight plans each defining a flight by an aircraft; the system determines, for each aircraft and its respective received flight plan, a three-dimensional region of potential conflict, representative both of the uncertainty in the position of the aircraft and of a region of air exclusion appropriate for the aircraft or for the respective received flight plan; and the system determines, on the basis of the determined regions of potential conflict, whether one of the received flight plans is in conflict with any of the other received flight plans.

Abstract: Systems and methods for providing air traffic control center data to aircraft is provided. In certain embodiments an avionics system includes a communication device configured to communicate with a data center and an air traffic control center; and a processing unit configured to execute machine readable instructions. In at least one embodiments, the machine readable instructions cause the processing unit to manage communications associated with the flight of an aircraft, wherein the communications are communicated through the communication device with the data center; distinguish identifying information received through the communication device, wherein the identifying information identifies at least one of the air traffic control center and associated aeronautical telecommunications network address; and establish a communication session with the air traffic control center using the identifying information received through the communication device.

Abstract: A system and method for managing vehicles on a road network can include a processor that performs operations including accessing a matrix of vehicle parameters of a plurality of communicating vehicles on the road network and representing the plurality of communicating vehicles in a graph with a plurality of nodes corresponding to the plurality of communicating vehicles and edges corresponding to the vehicle parameters. The system and method can include partitioning, with a processing device, the graph to reduce disruptions to the road network below a threshold level to support safe and efficient traffic flow and assigning one or more exclusion zones within the road network to each partition of the graph by associating the vehicle parameters for each vehicle.

Abstract: A method of generating a flight plan including a number N-1 of segments SGi, i being an integer number between 2 and N. Segment SGilinks an auxiliary departure position to an auxiliary arrival position according to a route. The route is a straight line defined by a list of auxiliary route positions. Each route is stored in a database onboard the aircraft. The method includes a coupled determination of an auxiliary arrival position that is part of the auxiliary positions of at least one of the routes and of a route followed by the segment SGi+1. The coupled determination is produced from an auxiliary departure position and a route Ri, followed by the segment SGi.

Abstract: A position determining voting system that uses Doppler information from an on-board weather radar to improve the system's accuracy and/or fault tolerance includes a comparison function and an error integration function. The comparison function is used to monitor the independent position sources for correct operation, comparing and identifying a position source that should not be used based on its relative error compared with the other position sources and their characteristics. The integration function provides corrections to relative position sources by integrating the data from multiple absolute position sources when they are mutually consistent.

Abstract: A method of predicting the trajectory of an aircraft is disclosed in this specification. The method involves predicting corrective adjustments that an aircraft flight management system is expected to make to follow a reference trajectory. A ground based system receives a reference trajectory that the aircraft flight management system intends to fly and predicts an actual trajectory using the predicted corrective adjustments. The actual trajectory predicted by the system differs from the reference trajectory in a free dimension that is not restrained in the reference trajectory.

Abstract: This application describes the software invented to control an electric motor system. The electric motor system is mounted on one or more aircraft main wheels or nose wheels to drive an aircraft independently on the ground without aircraft engines or tow vehicles. The software uses closed-loop control together with several other control laws to operate the drive motor or motors. Knowledge of the current operating state of the drive motor, together with knowledge of the commands given to taxi forward, taxi in reverse, or brake in reverse, is used to configure the motors to optimal operating parameters. The software architecture is described along with the pilot interface and many details of software implementation.

Abstract: The present invention takes the form of a computer program, method and/or system to allow an airline, aviation authority or other aviation entity to temporally manage, coordinate and allocate aircraft arrival/departure Slot Times during a specified period for the flow of a plurality of aircraft at a specified fix point, based upon specified data comprised of the aircraft, the fix point, associated system resources, business/operational goals, airline Requested Slot Times, Preferred Movement and aviation system specified criteria, some of which is temporally varying.

Abstract: A methods, apparatus and system are provided for a vehicle with a ground navigational display. The system may include a display, a navigation system determining a location of the vehicle, a database storing a map including locations of buildings on the map and a processor. The processor may be configured to display the map on the display based upon the location of the vehicle, assign a fixed height to all of the buildings displayed on the display, and render the buildings displayed on the display in three-dimensions and having the assigned fixed height.

Abstract: In one embodiment, a method comprises receiving, in a computer-based airspace monitoring system, airspace information from a plurality of different sources via a plurality of different communication networks, receiving, in the computer-based airspace monitoring system, a first flightpath parameter from a first aircraft at a first point in time, wherein the first flightpath parameter comprises at least one of a three-dimensional position parameter, a flight trajectory parameter, or a speed parameter, establishing, in the computer-based airspace monitoring system, a first defined airspace in a region proximate the first aircraft, processing, in the computer-based airspace monitoring system, the airspace information for the first defined airspace based on the first position parameter received from the first aircraft to define a first data set of airspace information relevant to the first aircraft, and transmitting the first dataset of airspace information from the computer-based airspace monitoring system to the

Abstract: Systems and methods for estimating time of arrival for vehicle navigation are described. One embodiment of a method includes determining a route for a vehicle to reach a destination from a current location determining, by the computing device, an estimated time for reaching the destination from the current location. Embodiments of the method additionally include determining, by the computing device, a current range of the vehicle, based on current fuel level and vehicle fuel efficiency and determining, by the computing device and based on the current range, whether the vehicle can reach the destination without refueling. Some embodiments include revising, by the computing device, the estimated time for reaching the destination to include a waypoint to refuel in response to determining that the vehicle cannot reach the destination without refueling and providing, by the computing device, the estimated time for reaching the destination for display to a user.

Abstract: A method for requesting air traffic control (ATC) clearance comprising receiving user input to display an ATC clearance request page corresponding to a respective flight parameter; based on the received user input, requesting a computed value for the respective flight parameter from a flight management (FMS) system; and displaying the computed value with the ATC clearance request page corresponding to the respective flight parameter.

Abstract: The invention is a system and method of compressing a DTM to be used in an Auto-GCAS system using a semi-regular geometric compression algorithm. In general, the invention operates by first selecting the boundaries of the three dimensional map to be compressed and dividing the three dimensional map data into regular areas. Next, a type of free-edged, flat geometric surface is selected which will be used to approximate terrain data of the three dimensional map data. The flat geometric surface is used to approximate terrain data for each regular area. The approximations are checked to determine if they fall within selected tolerances. If the approximation for a specific regular area is within specified tolerance, the data is saved for that specific regular area. If the approximation for a specific area falls outside the specified tolerances, the regular area is divided and a flat geometric surface approximation is made for each of the divided areas.

Abstract: Methods and apparatus are provided for an actively variable shock absorbing system for actively controlling the load response characteristics of a shock absorbing strut. In one embodiment the shock absorbing system comprises a controllable valve adapted for actively varying a load response characteristic of the shock absorbing strut. The shock absorbing system further comprises an electronic control system comprising an input for receiving a signal from a sensor, an algorithm adapted to determine an optimal position for the controllable valve in view of the sensor signal, and an output for sending a control signal to the controllable valve to place the valve in the optimal position.

Abstract: A system and method are provided to support accommodating safe integration of small unmanned aircraft systems (sUASs) into the National Airspace Structure in the United States. A specifically-tailored service is provided to address a change of paradigm from aircraft-based avionics/capabilities to a ground-based solution centered on the sUAS control station that is typically employed to manage an sUAS mission and/or flight. Appropriate software, server and system components are integrated into an interactive, easy-to-use, web-based tool that provides interested parties with real-time, graphical flight-following information to acquire position information regarding an sUAS platform from the control console for the sUAS platform. The acquired position information is forwarded to a separate server that can augment and provide graphical display of the sUAS intended route of flight (flight planned route).

Abstract: The present invention takes the form of a computer program, method and/or system to allow an airline, aviation authority or other aviation entity to temporally manage, coordinate and allocate aircraft arrival/departure Slot Times during a specified period for the flow of a plurality of aircraft at a specified fix point, based upon specified data comprised of the aircraft, the fix point, associated system resources, business/operational goals, airline Requested Slot Times, Preferred Movement and aviation system specified criteria, some of which is temporally varying.

Abstract: Methods and systems for determining a cyclical pattern of trajectories for a fleet of vehicles are provided. In one example, a method comprises receiving a sequence of coverage requirements for a region and an associated period of time. For each of one or more phases of the period of time, possible routes that a vehicle located at one or more respective landmarks at a beginning of the phase could follow to reach one or more additional landmarks by an end of the phase are determined. Further, a cyclical pattern of trajectories for vehicles of a fleet of vehicles that minimizes a difference between a distribution of the fleet at a beginning of the period of time and a distribution of the fleet at an end of the period of time is determined.

Abstract: An assist device for ensuring the accuracy and integrity of position information of an aircraft on the ground includes a processing unit for determining in the airport (AE) a zone (ZP) of insensitivity to multipath GPS signals, the zone (ZP) having a rectangular shape, which is determined relative to the threshold (O) of the runway, and which has a length (L1) equal to the length of the runway and a width (L2) depending on a maximum illumination distance (D). The device further includes a unit for verifying, while the aircraft is moving in the airport (AE), whether the position relative to position information of the aircraft is inside said runway zone (ZP). A method for ensuring the accuracy and integrity of position information of an aircraft on the ground is also disclosed herein.

Abstract: A present novel and non-trivial system, device, and method for presenting flight information of a plurality of aircraft on a display unit. An image generator (“IG”) is programmed to receive a first request for flight information for one of a plurality of aircraft; receive first flight information of a viewer aircraft when included in the request; send a second request for second flight information of a target aircraft for each target aircraft included in the request; receive the second flight information; retrieve terrain data corresponding the flight information of a focal aircraft; generate an image data set representative of a three-dimensional scene of a selectable view comprised of the sky, the spherical surface of the Earth, a first aircraft symbol corresponding to the received flight information, and a first curved flight path; and provide the image data set to a display unit.

Abstract: A device for determining ageing of a hydraulic fluid in a hydraulic system with a multitude of hydraulic components is provided. The device comprises at least one temperature determination device and at least one ageing determination device, wherein the temperature determination device determines the respective temperature of each discrete fluid volume of the hydraulic fluid in the hydraulic system, and from the aforesaid the ageing determination device determines an increase in ageing. Generally, the temperature determination device carries out a numerical thermal simulation of the hydraulic system, component by component, including determining at least one temperature of at least one hydraulic component of the hydraulic system, which simulation is supported by measuring the temperatures of individual hydraulic components by means of temperature sensors.

Abstract: Example methods and systems for decomposing fleet planning optimizations via spatial partitions are described. An example method includes receiving information indicating a sequence of coverage requirements for a region over a period of time. The region is characterized by a plurality of landmarks and the period of time is divided into a plurality of phases. An individual coverage requirement indicates a desired number of vehicles of a plurality of vehicles for respective landmarks at a given phase. The method also includes dividing the region into a plurality of sub-regions, and determining sub-region fleet plans for the plurality of sub-regions based on estimates of one or more vehicles entering respective sub-regions and estimates of one or more vehicles leaving respective sub-regions. The method also includes combining the sub-region fleet plans to produce a fleet plan responsive to the sequence of coverage requirements for the region.

Abstract: A system and method according to which travel data is received, a projected times forecast is generated using the travel data, a probable times forecast is generated using the projected times forecast, and a postable times forecast is generated using the probable times forecast. In an exemplary embodiment, the travel data is airline flight data.

Abstract: A system and method for managing transportation transactions according to which one or more vehicles such as, for example, airplanes, depart from a specific location such as, for example, an airline gate.

Abstract: A method and apparatus for providing a traffic information service using a mobile communication terminal are provided. A method of a mobile communication terminal for a traffic information service is provided. The method includes constructing a cluster with at least one neighboring Mobile Station (MS), receiving traffic information from the at least one neighboring MS comprised in the cluster, measuring traffic information using location information of the MS, and transmitting a traffic information message comprising the collected traffic information to a traffic information provision server.

Abstract: An airspace complexity reducing system is provided. The airspace complexity reducing system has a data storage device including data describing a multivariable model of an airspace complexity, the airspace complexity being a cumulative effect of factors that influence a system user's ability to manage aircraft in an associated airspace. The airspace complexity reducing system also has a selecting module configured to select a variable from a plurality of variables of the multivariable model and determine an amount by which to modify the selected variable to achieve a predetermined airspace complexity value. In addition, the airspace complexity reducing system has a suggestion module configured to determine a modification to the airspace that results in the determined variable modification and transmit the determined course of action to the system user.

Abstract: A method for displaying stop bar information to an aircrew member of an aircraft includes the steps of capturing a light signature emitted from an area surrounding the aircraft, processing the captured light signature to detect a lighted stop bar, and providing information to the aircrew member regarding the detection of the lighted stop bar.

Abstract: An aircraft traffic alert system that minimizes false alarms and unnecessary alerts by automatically adjusting the sensitivity of the system based on proximity to an airport. The system also can use information from a flight management system (FMS) or GPS navigation system (GNS) to only adjust the sensitivity near a destination airport and to suppress potential alerts for possible collisions with other aircraft that will be moot based on planned course changes of the subject aircraft. The system also can suppress alerts related to another aircraft when the other aircraft is landing on a parallel runway to the runway on which the subject aircraft is landing. The system may use multiple sensitivity levels based on different airspace classes, each class being associated with a different sensitivity level.

Abstract: A method of optically locating and guiding a vehicle relative to an airport having standardized signage where the method includes generating an image of at least a portion of the airport from an optical sensor mounted on the vehicle, determining the location of the vehicle, and providing guidance for operation of the vehicle.

Abstract: Embodiments of the present invention relate to avionics systems, and more particularly, to collision avoidance systems. In one embodiment, a system is delineated comprising a plurality of detection zones for a plurality of aircraft and means for issuing a report based on one or more of the plurality of detection zones.

Abstract: A system and methods for coordinating positioning of vehicles in motion is disclosed. The method graphically presents displayed synchronization parameters on a display screen such that a user determines a planned position of a first vehicle on a planned path in order to arrive at a predetermined position at a correct time. The method further synchronizes the first vehicle with the planned position on the planned path using the displayed synchronization parameters and performs a rendezvous between the first vehicle and a second vehicle.

Abstract: A method of detecting conflicts between aircraft passing through managed airspace, and to resolving the detected conflicts strategically. Air traffic control apparatus arranged to manage airspace through which aircraft are flying is provided that comprises processing means configured to receive aircraft intent data describing an aircraft's intended flight path, to launch a conflict detection procedure in which it computes a user-preferred trajectory for each of the aircraft based on the aircraft intent and determines whether any conflicts will arise, to launch a conflict resolution procedure in which it calculates revisions of the aircraft intent of the conflicted aircraft to remove the conflicts, and to transmit to the aircraft the revised aircraft intent data.

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: A departure sequencing system models airport operations and provides suggested gate pushback times for aircraft. In various embodiments, a departure sequencing system includes an airport state analyzer, a taxi-out predictor, and a pushback optimizer. The departure sequencing system may utilize stochastic models, and resolve aircraft conflicts using a business rules engine. Via use of the departure sequencing system, taxi times may be reduced, taxi fuel burn may be reduced, and airport throughput may be increased.

Abstract: A method for testing states in a flight plan state management system is provided, which includes defining control variables for monitoring the flight plan state management system, modeling the flight plan state management system based on the control variables defined for monitoring, calculating and extracting control variables for testing the stability of, and checking for errors in, the flight plan state management system using the result of modeling, testing the stability of, and checking for errors in, the flight plan state management system based on the calculated and extracted control variables for testing stability and checking for errors, and expressing the result of stability testing and error checking on a display panel.