[5] [5] Arzelier D, Peaucelle D. Robust impulse-to-peak synthesis: application to the control of an aerospace launcher［C］// International Conference on Robotics and Automation. IEEE, 2004.

[6] [6] D Arzelier, D Pe aucelle. Multiob jective H2/H∞impulse-to-peak synthesis: Application to the control of an aerospace launcher［C］. Proceedings of the 16th IFAC Symposium on Automatic Control inAerospace, St. Petersburg, June 2004.

[7] [7] D Peaucelle, D Arzelier, O Bachelier, et al. A new robust D-stability condition for real convex polytopic uncertainty［J］. Systems & Control Letters, 2000, 40(1): 5-8.

[8] [8] J C Geromel, M C de Oliveira, L Hsu. LMI Characterization of structural and robust stability［J］. Linear Algebra and its Applications, 1998, 285(1-3): 69-80.

[9] [9] M.C. de Oliveira, J.C. Geromel, L. Hsu. LMI Characterization of structural and robust stability: thediscrete-time case［J］. Linear Algebra and its Applications, 1999, 296(1-3): 27-38.

[11] [11] O Voinot, P Apkarian, D Alazard. Gain-scheduling H∞ control of the launcher in atmosphericflight via linear-parameter varying technique［C］. AIAA Guidance, Navigation and Control Conference, Monterey, California, August 2002.