Electronics Optics & Control, Volume. 21, Issue 7, 81(2014)
Roll Control and Robustness Analysis for Hypersonic Vehicle in Reentry Phase
[1] [1] CALHOUN P.An entry flight controls analysis for a reu-sable launch vehicle [R].AIAA-2000-1046, 2000.
[2] [2] MOUL M T, PAULSON J W.Dynamic lateral behavior of high-performance aircraft[R].NACA RM-L58E16, 1958.
[3] [3] LEE H P, CHANG M, KAISER M K.Flight dynamics and stability and control characteristics of the X-33 technology demonstrator vehicle[R].AIAA-98-4410, 1998.
[4] [4] WU L N, HUANG Y M, HE C L.Research on lateral control system for reusable launch vehicle in return phase[J].Journal of Nanjing University of Aeronautics & Astronautics, 2009, 41(3):329-333.
[5] [5] KUREEMUN R, BATES D G, HAYES M J.On the gene-ration of LFT-based uncertainty models for flight control law robustness analysis[R].AIAA-2001-4396, 2001.
[6] [6] TU K Y, SIDERIS A, MEASE K D, et al.Robust lateral-directional control design for the F/A-18[R].AIAA-1999-4204, 1999.
[7] [7] GREGORY I, MCMINN J, SHAUGHNESSY J.Hypersonic vehicle control law development using H∞ and μ-synthesis[R].AIAA-1992-5010, 1992.
[8] [8] LIU L.Method of assessment and confirmation for modern flight control system[M].Beijing:National Defense Industry Press, 2010.
[9] [9] MORTON B, MCAFOOS R.A u-test for real parameter variations[C]//Proceeding of the ACC, 1985:135-138.
Get Citation
Copy Citation Text
LIU Jun, HUANG Yi-min, SUN Chun-zhen, YIN Liang-liang. Roll Control and Robustness Analysis for Hypersonic Vehicle in Reentry Phase[J]. Electronics Optics & Control, 2014, 21(7): 81
Category:
Received: Aug. 12, 2013
Accepted: --
Published Online: Jul. 10, 2014
The Author Email: