본문 바로가기 주메뉴 바로가기
국회도서관 홈으로 정보검색 소장정보 검색

목차보기

Contents

Development of flight control law for improvement of uncommanded lateral motion of the fighter aircraft / Chong-Sup Kim ; Chang-Ho Ji ; Byoung Soo Kim 1

Abstract 1

Abbreviations 1

1. Introduction 2

2. Control Law Design 4

2.1. Inverse Model 6

2.2. Desired Dynamics 6

2.3. Additional Augmentation Control 7

3. Flying Quality parameter Optimization and Control Law Analysis 8

3.1. Analysis Points and Items 8

3.2. Optimization of Flying Quality Parameter 8

3.3. Frequency-Domain Linear Analysis 9

3.4. Time-Domain Nonlinear Simulation 12

4. Conclusions 14

5. Future Works 15

Appendix 15

References 18

권호기사

권호기사 목록 테이블로 기사명, 저자명, 페이지, 원문, 기사목차 순으로 되어있습니다.
기사명 저자명 페이지 원문 목차
Effect of external heat input on fluid sloshing dynamic performance in a liquid oxygen tank Zhan Liu, Yuyang Feng, Yuanliang Liu, Jia Yan, Yanzhong Li p. 879-888

보기
Numerical research on the unsteady evolution characteristics of blade tip vortex for helicopter rotor in forward flight Zhou Ye, Fengjiang Zhan, Guohua Xu p. 865-878

보기
Online safe flight envelope protection for icing aircraft based on reachability analysis Zhilong Yu, Yinghui Li, Zhe Zhang, Wenfeng Xu, Zehong Dong p. 1174-1184

보기
Nonlinear flight mode identification by applying modified ensemble empirical mode decomposition and Hilbert-Huang transformation S. Abolfazl Mokhtari, Mehdi Sabzehparvar, Kazem Imani p. 1161-1173

보기
CFDP PDU tunneling service over DTN between heterogeneous deep space communication assets Cheol Hea Koo, Hyungshin Kim p. 1147-1160

보기
Optimal lunar point return orbit design and analysis via a numerical three-step approach Yongjun Song, Young-Joo Song, Kap-Sung Kim, Ho Jin, Donghun Lee p. 1129-1146

보기
Performance evaluation on packet transmission for AFDX networks using optimized forward end-to-end delay analysis Qingfei Xu, Xinyu Yang p. 1114-1128

보기
Global path planning of lunar rover under static and dynamic constraints Ji Hoon Bai, Young-Jae Oh p. 1105-1113

보기
Intercept point prediction of ballistic missile defense using neural network learning Jun-Yong Lee, Byeong-Un Jo, Gun-Hee Moon, Min-Jea Tahk, Jaemyung Ahn p. 1092-1104

보기
Guidance to control arrival angle and altitude for an unpowered aerial vehicle Seunghan Lim, Sungbong Cho, Eunyong Lee p. 1078-1091

보기
Development of flight control law for improvement of uncommanded lateral motion of the fighter aircraft Chong-Sup Kim, Chang-Ho Ji, Byoung Soo Kim p. 1059-1077

보기
Flight control design using incremental nonlinear dynamic inversion with fixed-lag smoothing estimation Tito J. Ludeña Cervantes, Seong H. Choi, Byoung S. Kim p. 1047-1058

보기
Effects of the O/F ratio on the performance of a low thrust LOx/methane rocket engine with an ElecPump-fed cycle Byungil Yu, Hyun-Duck Kwak, Hong Jip Kim p. 1037-1046

보기
Performance parameter analysis of a Hall effect thruster with modified Bohm parameter model Min Gyoung Cho, Gwanyong Jung, Hong-Gye Sung p. 1028-1036

보기
(The) selective zero emission power systems between NaBH4-based fuel cells and solar cells for UAVs Byeong Gyu Gang p. 1017-1027

보기
Nonlinear aeroelastic analysis of heated curved panels in supersonic air flow Jian Zhou, Minglong Xu, Zhichun Yang p. 996-1016

보기
(The) damage criterion affecting life prediction of fiber-reinforced Al-Li alloy laminates under spectrum loading Weiying Meng, Yupeng Li, Xiaochen Zhang, Huaitao Shi, Yu Zhang, Xiao Lv p. 984-995

보기
Flight test applications of an improved operational load monitoring device Chan Yik Park, Myung-Gyun Ko, Sang-Yong Kim, Jae-Seok Ha p. 970-983

보기
(An) equivalent modeling method for honeycomb sandwich structure based on orthogonal anisotropic solid element Jian Yuan, Lei Zhang, Zhanwei Huo p. 957-969

보기
Nozzle flow influence on forebody aerodynamics Sangha Park, Gisu Park, Soo Hyung Park p. 942-956

보기
Assessment of cavity covered with porous surface in controlling shock/boundary-layer interactions in hypersonic intake Tamal Jana, T. Thillaikumar, Mrinal Kaushik p. 924-941

보기
Effect of shape of two-dimensional smooth hump on boundary layer instability Donghun Park, Sejong Oh p. 906-923

보기
Ablation experiments of ultra-high-temperature ceramic coating on carbon-carbon composite using ICP plasma wind tunnel Rajesh Kumar Chinnaraj, Seong Min Hong, Ho Seok Kim, Phil Yong Oh, Seong Man Choi p. 889-905

보기

참고문헌 (53건) : 자료제공( 네이버학술정보 )

참고문헌 목록에 대한 테이블로 번호, 참고문헌, 국회도서관 소장유무로 구성되어 있습니다.
번호 참고문헌 국회도서관 소장유무
1 ChambersJR, Hall RM Historical review of uncommanded lateraldirectional motions at transonic conditions. In: 41st aerospace sciences meeting & Exhibit, 6–9 January 2003. 미소장
2 Hall RM, Woodson SHIntroduction to the Abrupt Wing Stall (AWS) Program. In: American Institute of Aeronautics and Astronautics Journal of Aircraft, Vol. 41, No. 3, May–June 2004. 미소장
3 Owens DB, McConnell JK, Brandon JM, Hall RM Transonic freeto-roll analysis of the F/A-18E and F-35. In: American institute of aeronautics and astronautics atmospheric flight mechanics conference and exhibit, 16–19 August 2004. 미소장
4 Anderson SB, Ernst EA, Van Dyke RD Flight measurements of the wing-dropping tendency of a straight-wing jet airplane at high subsonic mach numbers. In: NACA RM A51 628, 1951. 미소장
5 McFadden NM, Rathert GA, Bray RS, The eff ectiveness of wing vortex generators in improving the maneuvering characteristics of a swept-wing airplane at transonic speeds, NACA TN 3523, 1955. 미소장
6 The eff ects of buff eting and other transonic phenomena on maneuvering combat aircraft, Advisory Group for Aerospace Research and Development, July 1975. 미소장
7 Rahn R oversimplifi cation can sometimes be hazardous to your health-the XA4D skyhawk story. In: Society of experimental test pilots symposium. 미소장
8 Phillips EH Team correcting defi ciencies in Navy’s T-45A trainer aircraft, Aviation Week and Space Technology, October 30, 1989. 미소장
9 Friend EL, Sefic WJ (August 1972) Flight Measurements of Buffet Characteristics of the F-104 Airplane for Selected Wing-Flap Defl ections, NASA TN D-6943. National Aeronautics and Space Administration, Washington 미소장
10 MonaghanRC, Friend EL (1973) Eff ects of flaps on buff et characteristics and wing-rock onset of an F-8C airplane at subsonic and transonic speeds”, NASA TM X-2873 미소장
11 HanleyRJ (1987) Development of an airframe modifi cation to improve the mission eff ectiveness of the EA-68 airplane, American Institute of Aeronautics and Astronautics , 87–2358. 미소장
12 ChambersJR, Anglin EL (1969) Analysis of lateral-directional stability characteristics of a twin-jet fighter airplane at high angles of attack, NASA TN D-5361. 미소장
13 RayEJ, Hollingsworth EG (1973) Subsonic characteristics of a twin-jet swept-wing fighter model with maneuvering devices. 미소장
14 Manoeuvre Limitations of Combat Aircraft, AGARD Advisory Report No. 155A. 1979. 미소장
15 HwangC, Pi WS (1974) Investigation of northrop F-5A wing buff et intensity in transonic flight, NASA Contractor Report 2484. 미소장
16 HwangC, Pi WS (1978) Investigation of steady and fluctuating pressures associated with the transonic buff eting and wing rock of a one-seventh scale model of the F-5A aircraft, NASA Contractor Report 3061. 미소장
17 Hwang C, PiWS (2012) Some observations on the mechanism of aircraft wing rock. In: American institute of aeronautics and astronautics aircraft systems and technology conference, Los Angeles, CA. 미소장
18 LusbyWA, Hanks NJ (1961) T-38A category II stability and control tests, AFFTC-TR-61–15. 미소장
19 FriendEL, Sakamoto GM (1978) Flight comparison of the transonic agility of the F-111A airplane and the F-111 supercritical wing airplane, NASA TP 1368. 미소장
20 Bore CL Post-stall aerodynamics of the harrier GRl, AGARDCP-102 fluid dynamics of aircraft stalling 미소장
21 MossGF Some UK research studies of the use of wing-body strakes on combat aircraft confi gurations at high angles of attack 미소장
22 Stevenson SL, Holl D, Roman A (1992) Parameter identifi cation of AV-86 wingborne aerodynamics for flight simulator model updates, American Institute of Aeronautics and Astronautics 92–4506-CP. 미소장
23 O’Leary CO (1977) Wind-tunnel measurement of lateral aerodynamic derivatives using a new oscillatory rig with results for the gnat aircraft. RAE Tech Rep 771:59 미소장
24 SiskTR, Matheny NW (1979) Precision controllability of the F-15airplane, NASA technical memorandum TM-72861. 미소장
25 DavisonMT (1992) An examination of wing rock for the F-15. master’s thesis, Air Force Institute of Technology, AFIT/GAE/ENY/92M-O11, February. 미소장
26 Sisk TR, Matheny NW (1980) Precision controllability of the YF-17 airplane, NASA Technical Paper TP-1677. 미소장
27 Traven R, Hagan J, Niewoehner R, Solving Wingdrop on the F-18E/F Super Hornet. In: Proceedings of the 42nd symposium aerospace and high technology database, society of experimental test pilots, Lancaster, CA, Sept. 1998, pp. 67–84. 미소장
28 Luo J, Lan EC (1993) Control of the wing rock motion of slender delta wings. J Guidance Control Dyn 16(2):225–231 미소장
29 Shue SP, Sawan ME, Rokhsaz K (1996) Optimal feedback control of a nonlinear system: wing rick example. J Guidance Control Dyn 19(1):166–171 미소장
30 Singh SN, Yim W, Wells WR (1995) Direct adaptive and neural control of wing-rock motion of slender delta wings. J Guidance Control Dyn 18(1):25–30 미소장
31 Monahemi MM, Kristic M (1996) Control of wing rock motion using adaptive feedback linearization. J Guidance Control Dyn 19(4):905–912 미소장
32 Hsu L (1990) Variable structure model reference adaptive control using only input and output measurements: the general case. In:IEEE transactions on automatic control, Vol. AC-35, No. 11, pp. 1238–1243. 미소장
33 Hsu L, Araujo AD, Costa RR Analysis and design of I/O based variable structure adaptive control. In: IEEE Transactions on Automatic Control, Vol. AC-39, No. 1, 1994, pp. 4–21. 미소장
34 Narendra KS, Annaswamy A (1989) Stable adaptive systems. Prentice-Hall, Upper Saddle River 미소장
35 de AraujoAD, Singh SN (1997) Variable structure adaptive control of wing-rock motion of slender delta wings, AIAA-97–3488. 미소장
36 Walker GP, Allen DA (2002) X-35B STOVL flight control law design and flying qualities. In: 2002 biennial international powered lift conference and exhibit, Williamsburg, Virginia, USA. November 5–7 미소장
37 Enns DF, Bugajski DJ, Carter J, Antoniewicz B (1994) Multiapplication controls—roust nonlinear multivariable aerospace controls applications. In: 4th NASA high alpha conference. 미소장
38 Munday S (2000) X-38 MACH FCS Overview. SAE Aerospace G&C, March 16. 미소장
39 Brinker JS, Wise KA (2001) Flight testing of reconfi gurable control law on the X-36 tailless aircraft. J Guidance Control Dyn 24(5):903–909 미소장
40 Wacker R, Munday S, Merkle S (2001) X-38 application of dynamic inversion flight control. In: 24th annual AAS guidance and control conference, Breckenridge, CO, USA, January 31Febrary 4. 미소장
41 Ito D, Georgie J, Valasek J, Ward DT (2002) Reentry vehicle flight controls design guidelines: dynamic inversion, NASA/TP-2002–210771. 미소장
42 Miller CJ (2011) Nonlinear dynamic inversion baseline control law: flight-test results for the full-scale advanced systems testbed F/A-18 airplane. In: American institute of aeronautics and astronautics, guidance, navigation, and control conference, August 8–11. 미소장
43 Integration – gestern, heute und morgen 네이버 미소장
44 Smith P, Berry A (2000) Flight test experience of a non-linear dynamic inversion control law on the VAAC harrier. In: Atmospheric flight mechanics conference. 미소장
45 Smith PR (1998) A simplifi ed approach to non-linear dynamic inversion based flight control. In: Proc. of the 1998 American institute of aeronautics and astronautics, atmospheric flight mechanics conference, pp 762-770 미소장
46 Lu K, Liu C L1 adaptive control scheme for UAV carrier landing using nonlinear dynamic inversion. In: international journal of aerospace engineering Volume 2019, Article ID 6917393, 8 pages 미소장
47 Department of Defense Handbook Flying Qualities of Piloted Aircraft, MIL-HDBK-1797, 19 December 1997. 미소장
48 Kim CS, Yang I, Koh G-o, Kim B-s (2018)development of the model-/sensor-based nonlinear dynamic inversion control technique for highly maneuverability fighter. In: Institute of Control, Robotics and Systems, vol. 24, no. 7, pp. 639–654. 미소장
49 Flight Control Systems - Design, Installation and Test of Piloted Aircraft, General Specifi cation for, MIL-DTL-9490E, 22, April, 2008. 미소장
50 Cook S, Bachner S, Imhof G (2002) Assessing the impact of uncommanded lateral motion using simulation. In: Proceedings of the NATO RTO/SCI symposium- challenges in dynamics, system identifi cation, control and handling qualities for land, air, sea and space vehicles, Berlin, May. 미소장
51 Cook MV (2007)Flight Dynamics Principles, Elsevier aerospace engineering series. 미소장
52 Berger T, Tischler MB Lateral/Directional control law design and handling qualities optimization for a business jet flight control system. In: American institute of aeronautics and astronautics atmospheric flight mechanics conference, August 19–22 2013, Boston, MA. 미소장
53 Consultancy Report—Intermediate control law analysis and design, NLR, September, 2019. 미소장