| Citation: | TU Zhangjie, WANG Lixin, CHEN Junpinget al. Assessment of go-around climb gradient for civil aircraft based on digital virtual flight[J]. Journal of Beijing University of Aeronautics and Astronautics, 2017, 43(12): 2530-2538. doi: 10.13700/j.bh.1001-5965.2016.0879(in Chinese)
|
The climb gradient of the aircraft reflects its ability of flying over the ground barrier to a safe altitude. To ensure safety of civil aircraft when going around, airworthiness regulations provide that the go-around climb gradient should meet certain numerical requirements. According to provisions of airworthiness regulations on go-around procedure and go-around climb gradient of civil aircraft, an airworthiness compliance assessment method of go-around climb gradient was proposed based on digital virtual flight. The task digitized model of go-around and pilot control model were established based on the airworthiness regulations as well as the characteristics of pilot control. Then the flight dynamics model of a certain domestic turbojet aircraft was established, which eventually constituted digital virtual flight simulation system for go-around task. The climb gradient evaluations of landing climb and approach climb were completed by flight simulation. Compared with the real flight test results, the evaluation errors are less than 10%, which verifies the applicability and accuracy of the method. This method can be applied to the design of civil aircraft, so as to provide support for determining the airworthiness compliance of go-around climb performance and the maximum landing weight of aircraft.
| [1] |
刘彦俊.复飞的分析与探讨[J].空中交通管理, 2011(6):15-17. http://www.cqvip.com/QK/86849X/201106/38376161.html
LIU Y J.Analysis and discussions on missed approach[J].Air Traffic Management, 2011(6):15-17(in Chinese). http://www.cqvip.com/QK/86849X/201106/38376161.html
|
| [2] |
中国民用航空局. 中国民用航空规章第25部: 运输类飞机适航标准: CCAR-25-R4[S]. 北京: 中国民用航空局, 2011.
Civil Aviation Administration of China.China civil aviation regulations Part 25:Airworthiness standards of transport category aircraft:CCAR-25-R4[S].Beijing:Civil Aviation Administration of China, 2011(in Chinese).
|
| [3] |
田勇, 万莉莉.飞机性能工程学[M].北京:科学出版社, 2015.
TIAN Y, WAN L L.Aircraft performance engineering[M].Beijing:Science Press, 2015(in Chinese).
|
| [4] |
FILIPPONE A.Flight performance of fixed and rotary wing aircraft[M].Berlin:Elsevier, 2006.
|
| [5] |
蒋苗, 吴洋.CJ818高原起降单发失效爬升梯度分析[J].民用飞机设计与研究, 2009(S1):45-49. http://kns.cnki.net/KCMS/detail/detail.aspx?filename=myfj2009s1009&dbname=CJFD&dbcode=CJFQ
JIANG M, WU Y.Analysis of single failure climbing gradient of CJ818 plateau taking off and landing[J].Civil Aircraft Design and Research, 2009(S1):45-49(in Chinese). http://kns.cnki.net/KCMS/detail/detail.aspx?filename=myfj2009s1009&dbname=CJFD&dbcode=CJFQ
|
| [6] |
JOHNSON S C, GLOVER H.Method for determining a currently obtainable climb gradient of an aircraft:U.S.Patent 6, 691, 004[P].2004-02-10.
|
| [7] |
FILIPPONE A.Theoretical framework for the simulation of transport aircraft flight[J].Journal of Aircraft, 2010, 47(5):1679-1696. doi: 10.2514/1.C000252
|
| [8] |
孟祥光, 王立新, 刘海良.民机起飞爬升梯度适航符合性数学仿真评估[J].北京航空航天大学学报, 2016, 42(10):2222-2230. http://bhxb.buaa.edu.cn/CN/abstract/abstract13937.shtml
MENG X G, WANG L X, LIU H L.Mathematical simulation and assessment of airworthiness compliance of climb gradient during take-off of civil aircraft[J].Journal of Beijing University of Aeronautics and Astronautics, 2016, 42(10):2222-2230(in Chinese). http://bhxb.buaa.edu.cn/CN/abstract/abstract13937.shtml
|
| [9] |
BURDUN I Y, DELAURENTIS D A, MAVRIS D N.Modeling and simulation of airworthiness requirements for an hsct prototype in early design:AIAA-1998-4936[R].Reston:AIAA, 1998.
|
| [10] |
SCHARL J, MAVRIS D N, BURDUN I Y.Use of flight simulation in early design:Formulation and application of the virtual testing and evaluation methodology[C]//World Aviation Conference, 2000:5590.
|
| [11] |
XU H J, LIU D L, XUE Y, et al.Airworthiness compliance verification method based on simulation of complex system[J].Chinese Journal of Aeronautics, 2012, 25(5):681-690. doi: 10.1016/S1000-9361(11)60434-2
|
| [12] |
刘海良, 王立新.基于数字虚拟飞行的民用飞机纵向地面操稳特性评估[J].航空学报, 2015, 36(5):1432-1441. http://kns.cnki.net/KCMS/detail/detail.aspx?filename=hkxb201505006&dbname=CJFD&dbcode=CJFQ
LIU H L, WANG L X.Assessment of longitudinal ground stability and control for civil aircraft based on digital virtual flight testing method[J].Acta Aeronautica et Astronautica Sinica, 2015, 36(5):1432-1441(in Chinese). http://kns.cnki.net/KCMS/detail/detail.aspx?filename=hkxb201505006&dbname=CJFD&dbcode=CJFQ
|
| [13] |
LIU F, WANG L, TAN X.Digital virtual flight testing and evaluation method for flight characteristics airworthiness compliance of civil aircraft based on HQRM[J].Chinese Journal of Aeronautics, 2015, 28(1):112-120. doi: 10.1016/j.cja.2014.12.013
|
| [14] |
美国联邦航空局. 飞机飞行手册[M]. 陈新河, 译. 上海: 上海交通大学出版社, 2010: 298-299, 301.
United States Federal Aviation Administration.Aircraft flight manual[M].CHEN X H, translated.Shanghai:Shanghai Jiao Tong University Press, 2010:298-299, 301(in Chinese).
|
| [15] |
修忠信, 由立岩.运输类飞机合格审定飞行试验指南[M].上海:上海交通大学出版社, 2013:56.
XIU Z X, YOU L Y.Flight test guide for certification of transport category airplanes[M].Shanghai:Shanghai Jiao Tong University Press, 2013:56(in Chinese).
|
| [16] |
ETKIN B.Dynamics of flight:Stability and control[M].New York:John Wiley and Sons, 1995.
|
| [17] |
HEFFLEY R K.Use of a task-pilot-vehicle (TPV) model as a tool for flight simulator math model development:AIAA-2010-7620[R].Reston:AIAA, 2010.
|
| [18] |
JOHNSON E N, PRITCHETT A R.Generic pilot and flight control model for use in simulation studies[C]//AIAA Modeling and Simulation Technologies Conference and Exhibit.Reston:AIAA, 2002:4694.
|
| [19] |
贾重任, 黄成涛, 王立新.空中最小操纵速度的人机闭环数学仿真计算[J].北京航空航天大学学报, 2013, 39(5):580-584. http://bhxb.buaa.edu.cn/CN/abstract/abstract12606.shtml
JIA Z R, HUANG C T, WANG L X.Mathematical simulation method to calculate air minimum control speed[J].Journal of Beijing University of Aeronautics and Astronautics, 2013, 39(5):580-584(in Chinese). http://bhxb.buaa.edu.cn/CN/abstract/abstract12606.shtml
|
| [20] |
POOL D M, MULDER M, ZAAL P M T, et al.Pilot equation in manual control of aircraft dynamics[C]//Proceedings of the 2009 IEEE International Conference on Systems, Man and Cybernetics.Piscataway, NJ:IEEE Press, 2009:2480-2485.
|
| [21] |
HOSMAN R, VAN DER GEEST P, VAN DER ZEE J.Development of a pilot model for the manual balked landing maneuver:AIAA-2009-5818[R].Reston:AIAA, 2009.
|
| [22] |
ROBINSON J, BARNES S, WEBB M, et al.The use of pilot modeling in aviation reguatory affairs:AIAA-2009-5825[R].Reston:AIAA, 2009.
|
| [23] |
高金源, 李陆豫, 冯亚昌, 等.飞机飞行品质[M].北京:国防工业出版社, 2003.
GAO J Y, LI L Y, FENG Y C, et al.Aircraft handling qualities[M].Beijing:National Defend Industry Press, 2003(in Chinese).
|
Figures(8) / Tables(3)
Copyright © Journal of Beijing University of Aeronautics and Astronautics
Address: Editorial Department of Journal of Beijing University of Aeronautics and Astronautics, 37 Xueyuan Road, Haidian District, Beijing Post Code: 100191 Email: jbuaa@buaa.edu.cn
Supported by:
Beijing Renhe Information Technology Co., Ltd.
DownLoad:
