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95 results about "Flight schedule" patented technology

Predicating system and method for air dynamic traffic volume in terminal airspace

ActiveCN103530704AReduce workloadIncrease the level of regulatory automationForecastingAircraft traffic controlTraffic flowData acquisition module
The invention discloses a method for obtaining a basic operation volume of a terminal airspace. According to the method, a sector volume is amended by a human kinetic model and machine studying, and the basic operation volume of the terminal airspace can be accurately obtained. The invention also discloses a predicating method for the air dynamic traffic volume in the terminal airspace, and the traffic flow information and analysis for historical weather and predicating weather for the specific terminal airspace are increased, so the obtained volume predicating information of the terminal airspace is more accurate. The invention also discloses a predicating system for the air dynamic traffic volume in the terminal airspace; the system comprises a data collecting module, a data processing module, a control module and a display module; the system is used for realizing the method for obtaining the basic operation volume of the terminal airspace and realizing the predicating method for the air traffic volume in the terminal airspace. According to the predicating system and method for the air dynamic traffic volume in the terminal airspace, the effectiveness and accuracy for establishing a flight schedule of an airline are improved, and a basis is provided for an air traffic control unit to effectively determine the management and control of the air traffic in a pre-tactics stage according to the dynamic volume distribution.
Owner:NANJING UNIV OF AERONAUTICS & ASTRONAUTICS

Aviation hub emergency management and control method

ActiveCN103218681AStrong technical innovationSimple calculationResourcesAviationTime information
The invention relates to the technical field of communication and transportation design and management. Foundation support and a method are provided for a purpose that an aviation hub center specifically schedules and emergently manages. The adopted technical scheme is that an aviation hub emergency management and control method comprises a step of making a preliminary evaluation on an aviation hub comprehensive service level for a flight timetable influenced by real-time information such as possible abnormal states of airplanes and passengers. If the service level is not changed greatly, the timetable does not need to be optimized, and flying time is executed according to the timetable. If the service level is changed greatly, an emergency management plan is optimized and adjusted according to the flight timetable, the real-time information, specific characteristics and various restraints of the an aviation hub, and an optimized and adjusted timetable is fast worked out. Similarly, a preliminary evaluation of the aviation hub comprehensive service level is made for the timetable, if the service level is not improved, the timetable is continuous to be optimized, and if the service level is improved, the optimized and adjusted timetable is executed. At last, a comprehensive assessment is made on a practical implementation result. The aviation hub emergency management and control method is mainly applied to the planning design and management of the communication and transportation.
Owner:TIANJIN MUNICIPAL ENG DESIGN & RES INST

Realization system and method for airspace running simulation airflow engine

The invention provides a realization system and a method for airspace running simulation airflow engine. The realization system comprises a flight flow distribution feature analysis module, a flight flow statistics module, a flight flow factor modeling module and a simulation solution flight flow module, wherein, the flight flow distribution feature analysis module is used for determining the factor information of the flight flow, analyzing the distribution feature of each factor and determining the corresponding data probability model; the flight flow statistics module is used for accounting value of each factor in the current flight schedule according to the flight flow factor data probability model provided by the flight flow distribution feature analysis module, and determining the distribution parameters; the flight flow factor modeling module is used for respectively building the probability distribution model of each factor in the current flight schedule according to the data provided by the flight flow statistics module, and comprehensively forming the flight flow modeling model; the simulation solution flight flow module is used for generating the flight flow by simulation according to the requirements like the simulation flow rate input by users on the basis of flight flow factor modeling. The invention can improve the reasonability and validity of the generation of the flight flow data, thus creating conditions to ensure the reliability of the simulation flight assessment result and improve the credibility of the simulation assessment result.
Owner:AVIATION DATA COMM +1

Parallel runway capacity calculating method based on random simulation

InactiveCN106066906APrecise implementation managementReasonable Arrangement of Takeoff and Landing TimeGeometric CADDesign optimisation/simulationCapacity valueFlow management
The invention relates to a parallel runway capacity calculating method based on random simulation. The method includes the steps of setting initial parameters for calculating runway capacity, generating rising and landing type vectors of aircrafts, generating aircraft type vectors, allocating one corresponding arriving or departure point for each arriving or departing aircraft according to proportion, allocating one runway for each flight and generating runway vectors, sequentially calculating the interval Si, i+1 of i flight and i+1 flight from the first flight, calculating the taking-off and landing moments of each subsequent flight, calculating the flight number as the capacity value of current random conditions, taking a mean value as a runway capacity value after simulation for N times, and displaying the calculating result. Variable randomness is simulated through the monte-carlo method, and the taking-off and landing moments of each flight is calculated in a recursion way according to discrete event system principles. The capacity value is obtained by calculating the flight number in one hour. Scientific runway planning scheme evaluation is realized, and reasonable arrangement of flight schedule and precise flow management are realized.
Owner:CIVIL AVIATION UNIV OF CHINA
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