[1] LI D PHU Y AHE J X.The design of terminal sliding control system for vertical launching missile［J］.Journal of ProjectilesRocketsMissiles and Guidance200929(6): 9-11.

[2] SUN Y TDAI S W.Research on optimal control for vertically launching warship-to-air missiles［J］.Microcomputer Information201228(5):43-44.

[3] YIN Y XYANG MWANG Z C.Modeling and control of vertically launching parallel vehicle［J］.Journal of Beijing University of Aeronautics and Astronautics200834(4): 369-372376.

[4] WANG Y H.Design of lateral thrust and aerodynamicsblended control system based on ADRC［D］.Harbin:Harbin Institute of Technology2009.

[5] CHENG G C.Quaternion and its application［M］.Changsha:National Defense Sciense and Technology Press1991.

[6] AO B QLIN W S.Attitude maneuver control of vertical launching tactical missile based on error quaternion［J］.Journal of Astronautics200425(1):98-101.

[7] QIN LZHANG W DPAN F.Quaternion method for kinematics modeling of high attack-angle flying carrier［J］.Journal of North University of China200627(3):276-279.

[8] HAN J Q.Active disturbance rejection control and its application［J］.Control and Decision199813(1):19-23.

[9] CHEN J KSUN X XZHANG L.The UAV longitudinal channel control based on ADRC［J］.Journal of Air Force Engineering University20067(6):10-12.

[10] ZHANG RHAN J Q.Auto disturbance rejection controller based on neural networks［J］.Journal of System Simulation200012(2): 149-151.

[11] HAN J Q.Nonlinear states error feed-back—NLSEF［J］.Control and Decision199510(3):221-225.

[12] HAN J Q.Active disturbance rejection control technique—the technique estimating and compensating the uncertainties［M］.Beijing:National Denfense Industy Press2008:288-296.