scholarly journals Stochastic modeling of aircraft flight parameters in terminal control area based on automatic dependent surveillance-broadcast (ADS-B) data

2021 ◽  
Vol 1173 (1) ◽  
pp. 012053
Author(s):  
R Medianto ◽  
J Jusuf ◽  
R Oktafianto ◽  
R Atiqah ◽  
J Sembiring ◽  
...  
Keyword(s):  
Stochastic Modeling ◽  
Control Area ◽  
Terminal Control ◽  
Aircraft Flight ◽  
Flight Parameters

scholarly journals A Ground Control Station for the UAV Flight Simulator

2016 ◽  
Vol 10 (1) ◽  
pp. 28-32
Author(s):  
Sławomir Romaniuk ◽  
Zdzisław Gosiewski ◽  
Leszek Ambroziak
Keyword(s):  
Flight Simulator ◽  
Ground Control ◽  
C Language ◽  
Aircraft Flight ◽  
Ground Control Station ◽  
Flight Parameters

Abstract In the paper implementation of a ground control station for UAV flight simulator is shown. The ground control station software is in cooperation with flight simulator, displaying various aircraft flight parameters. The software is programmed in C++ language and utilizes the windows forms for implementing graphical content. One of the main aims of the design of the application was to simplify the interface, simultaneously maintaining the functionality and the eligibility. A mission can be planned and monitored using the implemented map control supported by waypoint list.

scholarly journals Modeling and optimization of the terminal control area with holding unit

PLoS ONE ◽  
2021 ◽  
Vol 16 (3) ◽  
pp. e0241204
Author(s):  
Yun-Xiang Han
Keyword(s):  
Job Shop ◽  
Job Shop Scheduling ◽  
Control Area ◽  
Optimization Models ◽  
Scheduling Problem ◽  
Terminal Control ◽  
Job Shop Scheduling Problem ◽  
Flight Data ◽  
Shop Scheduling ◽  
Additional Constraints

Aiming at the problem of resource allocation for departure flights at congested airports, this research explores the optimal configuration of holding units in the terminal control area (TCA). Similar to the job-shop scheduling problem, this problem is solved through a max-plus model with additional constraints. In particular, two optimization models are constructed, in which air segments, departure fixes and holding units are explicitly modeled. Based on the realistic airspace network selected, the proposed models are tested using actual flight data. The experimental results show that the models proposed have better qualities compared with the other methods.

scholarly journals Optimization of standard arrival procedures at Sheremetyevo airport using rnav path terminators

2021 ◽  
Vol 24 (6) ◽  
pp. 17-26
Author(s):  
G. A. Gasparyan ◽  
M. V. Kulakov
Keyword(s):  
Traffic Flow ◽  
Traffic Management ◽  
Probabilistic Method ◽  
Main Idea ◽  
Air Traffic Management ◽  
Control Area ◽  
Terminal Control ◽  
Flow Management ◽  
Traffic Flow Management ◽  
New Ideas

Holding patterns are established at international airports to make the arriving traffic flow smooth and efficient. One of the main aims of holding patterns is to extend the aircraft arrival route, which allows ATC units to arrange the sequence on the arrival routes more effectively. The article considers the current methods and offers new ideas to improve the efficiency of the inbound traffic flow management using Paths and Terminators concept with HA holding patterns for standard arrival routes at Sheremetyevo Airport. As the main idea for optimizing air traffic management on this stage and reducing the workload on the controller, it is proposed to create extra routes in addition to the existing ones which include holding patterns, that will be used when needed to ensure a well-ordered traffic. The probabilistic method is used to calculate the maximum capacity of existing and proposed arrival routes with holding patterns. The proposed options for restructuring the airspace of the Moscow Terminal Control Area with preserving waypoints of starting standard arrival routes are presented.

Research on the Terminal Aircraft Separations Based on the History Surveillance Data

2014 ◽  
Vol 496-500 ◽  
pp. 2899-2903
Author(s):  
Zheng Hong Xia ◽  
Wei Jun Pan ◽  
Rui Kang ◽  
Xiao Lin Luo
Keyword(s):  
Air Traffic ◽  
Surveillance Data ◽  
Terminal Control ◽  
The Third ◽  
Aircraft Flight ◽  
Direction Change ◽  
The Impact

The contradictions between unreasonable terminal aircraft flight separation and rapidly increasing air traffic are prominent. Researches on the terminal control separation allowance are of vita importance to enhance aerodrome capacity and reduce fight delay. Based on the actual Airport Surveillance Radar (ASR) data of certain airport whose capacity was the third one of China, the terminal aircraft separations algorithm was proposed in this paper. The impact of aerodrome capacity, departure landing sequence and direction change of runway on flight separation were discussed.

A Flight Evaluating System Using Flight Gear

2013 ◽  
Vol 347-350 ◽  
pp. 891-894
Author(s):  
Hua Min Zhang ◽  
Li Li
Keyword(s):  
Wireless Communication ◽  
Real Time ◽  
Flight Performance ◽  
Flight Data ◽  
The Real ◽  
Aircraft Flight ◽  
Ground Station ◽  
Flight Parameters

This paper describes a system for evaluating flight of fixed-wing aircraft. During the flight of an aircraft, flight parameters are obtained and transmitted to the ground station by means of wireless communication. These flight data are received by the ground station and are calculated so as to get the input of flight gear, by internet interfaces flight gear can simulate the real-time state of the aircraft on the ground. The system can be used to evaluate the flight performance of a fixed-wing aircraft.

Unmanned aircraft automatic flight control algorithm in a spin maneuver

2020 ◽  
Vol 92 (8) ◽  
pp. 1215-1224
Author(s):  
Tomasz Rogalski ◽  
Paweł Rzucidło ◽  
Jacek Prusik
Keyword(s):  
Automatic Control ◽  
Flight Control ◽  
Unmanned Aircraft ◽  
Control Algorithms ◽  
Content Type ◽  
Aircraft Flight ◽  
Control Precision ◽  
In Series ◽  
Flight Parameters ◽  
High Control

Purpose The paper aims to present an idea of automatic control algorithms dedicated to both small manned and unmanned aircraft, capable to perform spin maneuver automatically. This is a case of maneuver far away from so-called standard flight. The character of this maneuver and the range of aircraft flight parameters changes restrict application of standard control algorithms. Possibility of acquisition full information about aircraft flight parameters is limited as well in such cases. This paper analyses an alternative solution that can be applied in some specific cases. Design/methodology/approach The paper uses theoretical discussion and breakdowns to create basics for development of structures of control algorithms. Simplified analytical approach was applied to tune regulators. Results of research were verified in series of software-in-the loop, computer simulations. Findings The structure of the control system enabling aerobatic flight (spin flight as example selected) was found and the method how to tune regulators was presented as well. Practical implications It could be a fundament for autopilots working in non-conventional flight states and aircraft automatic recovery systems. Originality/value The paper presents author’s original approach to aircraft automatic control when high control precision is not the priority, and not all flight parameters can be precisely measured.

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