TY - GEN
T1 - Research on aircraft take-off and landing performance based on flight simulation
AU - Guo, An
AU - Zhou, Zhou
AU - Zhu, Xiaoping
N1 - Publisher Copyright:
© 2018 IEEE.
PY - 2018/10/5
Y1 - 2018/10/5
N2 - In order to comply with the existing performance standard requirements or specifications, a new computational method is proposed for take-off and landing performance, which deals with the characteristics of the high precision of calculation parameters in the process of take-off and landing by flight simulation technique. A systematic aircraft model is constructed in detail, including aerodynamic model, engine model, landing gear model, mass model and nonlinear motion equation model. According to flight performance calculation standards and pilot control specifications, the different take-off modes and landing process are studied. Besides, one engine inoperative (OEI) take-off, angle of attack (AoA) hold take-off, standard take-off, reject take-off and landing simulation process are designed. Finally, the corresponding performance computer software is developed to achieve the goal of accuracy and rapid calculation. Simulation result shows that standard take-off distance is related to specified speed, AoA hold take-off distance is longer than standard take-off which needs satisfy speed and AoA requirements, and this method is appropriate for calculating the specific aircraft take-off and landing performance.
AB - In order to comply with the existing performance standard requirements or specifications, a new computational method is proposed for take-off and landing performance, which deals with the characteristics of the high precision of calculation parameters in the process of take-off and landing by flight simulation technique. A systematic aircraft model is constructed in detail, including aerodynamic model, engine model, landing gear model, mass model and nonlinear motion equation model. According to flight performance calculation standards and pilot control specifications, the different take-off modes and landing process are studied. Besides, one engine inoperative (OEI) take-off, angle of attack (AoA) hold take-off, standard take-off, reject take-off and landing simulation process are designed. Finally, the corresponding performance computer software is developed to achieve the goal of accuracy and rapid calculation. Simulation result shows that standard take-off distance is related to specified speed, AoA hold take-off distance is longer than standard take-off which needs satisfy speed and AoA requirements, and this method is appropriate for calculating the specific aircraft take-off and landing performance.
KW - Aircraft system modeling
KW - Angle of attack (AoA) hold take-off
KW - Flight simulation
KW - Standard take-off
KW - Take-off and landing performance
UR - http://www.scopus.com/inward/record.url?scp=85056347736&partnerID=8YFLogxK
U2 - 10.1109/ICMA.2018.8484675
DO - 10.1109/ICMA.2018.8484675
M3 - 会议稿件
AN - SCOPUS:85056347736
T3 - Proceedings of 2018 IEEE International Conference on Mechatronics and Automation, ICMA 2018
SP - 737
EP - 742
BT - Proceedings of 2018 IEEE International Conference on Mechatronics and Automation, ICMA 2018
PB - Institute of Electrical and Electronics Engineers Inc.
T2 - 15th IEEE International Conference on Mechatronics and Automation, ICMA 2018
Y2 - 5 August 2018 through 8 August 2018
ER -