Aircraft Take-off and Landing Performance Calculation Method Based on Flight Simulation
In order to comply with the existing standard requirements or specifications, a new computational method for aircraft take-off and landing performance, which deals with the characteristics of the high precision of parameters in the process of take-off and landing based on flight simulation technique...
| Format: | Article |
|---|---|
| Language: | zho |
| Published: |
EDP Sciences
2019-06-01
|
| Series: | Xibei Gongye Daxue Xuebao |
| Subjects: | |
| Online Access: | https://www.jnwpu.org/articles/jnwpu/full_html/2019/03/jnwpu2019373p433/jnwpu2019373p433.html |
| _version_ | 1797428944998236160 |
|---|---|
| collection | DOAJ |
| description | In order to comply with the existing standard requirements or specifications, a new computational method for aircraft take-off and landing performance, which deals with the characteristics of the high precision of parameters in the process of take-off and landing based on flight simulation technique. The simulation model for a twin-engine normal layout aircraft is constructed in detail, including nonlinear motion equation, aerodynamic, engine, landing gear and dynamical mass model. According to performance calculation standard and pilot control specification for different take-off modes and landing stages, the simulation process for one engine inoperative(OEI) take-off, angle of attack(AoA) hold take-off, standard take-off, reject take-off and landing are designed, and corresponding performance computer software is developed to achieve the goal of accuracy as well as full parameters calculation. Compared with the existing methods, the computational complexity of this method is increased, the process is detailed, the parameters are increased, and more influencing factors can be analyzed quantitatively. Results show that OEI take-off distance is the longest, standard take-off is suitable for light aircraft, angle of attack hold take-off is appropriate in plateau or limited thrust. Landing distance is related to glide angle. Therefore, light aircraft landing can reduce the approach speed and increase the glide angle. |
| first_indexed | 2024-03-09T09:06:09Z |
| format | Article |
| id | doaj.art-900968d45045410fa25c9955e3f73727 |
| institution | Directory Open Access Journal |
| issn | 1000-2758 2609-7125 |
| language | zho |
| last_indexed | 2024-03-09T09:06:09Z |
| publishDate | 2019-06-01 |
| publisher | EDP Sciences |
| record_format | Article |
| series | Xibei Gongye Daxue Xuebao |
| spelling | doaj.art-900968d45045410fa25c9955e3f737272023-12-02T10:25:34ZzhoEDP SciencesXibei Gongye Daxue Xuebao1000-27582609-71252019-06-0137343344210.1051/jnwpu/20193730433jnwpu2019373p433Aircraft Take-off and Landing Performance Calculation Method Based on Flight Simulation0123School of Aeronautics, Northwestern Polytechnical UniversitySchool of Aeronautics, Northwestern Polytechnical UniversityScience and Technology of UAV Laboratory, Northwestern Polytechnical UniversitySchool of Aeronautics, Northwestern Polytechnical UniversityIn order to comply with the existing standard requirements or specifications, a new computational method for aircraft take-off and landing performance, which deals with the characteristics of the high precision of parameters in the process of take-off and landing based on flight simulation technique. The simulation model for a twin-engine normal layout aircraft is constructed in detail, including nonlinear motion equation, aerodynamic, engine, landing gear and dynamical mass model. According to performance calculation standard and pilot control specification for different take-off modes and landing stages, the simulation process for one engine inoperative(OEI) take-off, angle of attack(AoA) hold take-off, standard take-off, reject take-off and landing are designed, and corresponding performance computer software is developed to achieve the goal of accuracy as well as full parameters calculation. Compared with the existing methods, the computational complexity of this method is increased, the process is detailed, the parameters are increased, and more influencing factors can be analyzed quantitatively. Results show that OEI take-off distance is the longest, standard take-off is suitable for light aircraft, angle of attack hold take-off is appropriate in plateau or limited thrust. Landing distance is related to glide angle. Therefore, light aircraft landing can reduce the approach speed and increase the glide angle.https://www.jnwpu.org/articles/jnwpu/full_html/2019/03/jnwpu2019373p433/jnwpu2019373p433.htmlflight performanceaircraft takeoff and landingsimulation modelingaircraft modelsangle of attack hold takeoffstandard takeoffflight simulation |
| spellingShingle | Aircraft Take-off and Landing Performance Calculation Method Based on Flight Simulation Xibei Gongye Daxue Xuebao flight performance aircraft takeoff and landing simulation modeling aircraft models angle of attack hold takeoff standard takeoff flight simulation |
| title | Aircraft Take-off and Landing Performance Calculation Method Based on Flight Simulation |
| title_full | Aircraft Take-off and Landing Performance Calculation Method Based on Flight Simulation |
| title_fullStr | Aircraft Take-off and Landing Performance Calculation Method Based on Flight Simulation |
| title_full_unstemmed | Aircraft Take-off and Landing Performance Calculation Method Based on Flight Simulation |
| title_short | Aircraft Take-off and Landing Performance Calculation Method Based on Flight Simulation |
| title_sort | aircraft take off and landing performance calculation method based on flight simulation |
| topic | flight performance aircraft takeoff and landing simulation modeling aircraft models angle of attack hold takeoff standard takeoff flight simulation |
| url | https://www.jnwpu.org/articles/jnwpu/full_html/2019/03/jnwpu2019373p433/jnwpu2019373p433.html |