[1] Office of the Secretary of Defense. Unmanned aerial roadmap 2002—2027 [R].Washington, DC 20301: Office of the Secretary of Defense, 2002.
[2] KIS L, LANTOS B. Quadrotor control based on partial sensor data [C]. Proceedings of the 19th International Workshop on Robotics in Alpe-Adria-Danube Region, Budapest, 2010.
[3] SHARIFI F, MIRZAEI M, GORDON B W, et al.. Fault tolerant control of a quadrotor UAV using sliding mode control [C]. Proceeding of the 2010 Conference on Control and Fault Tolerant Systems, Nice, 2010.
[4] CASTILLO P, LOZANO R, DZUL A. Stabilization of a mini rotorcraft with four rotors [J].IEEE Control Systems Magazine, 2005, 25(6): 45-55.
[5] DAS A, SUBBARAO K, LEWIS F. Dynamic inversion with zero-dynamics stabilization for quad-rotor control [J].IET Control Theory Applications, 2009, 3(3): 303-314.
[6] ZUO Z. Trajectory tracking control design with command-filtered compensation for a quadrotor [J]. IET Control Theory Applications, 2010, 4(11): 2343-2355.
[9] HOU Z C, GONG X, BAI Y, et al.. Robust trajectory tracking control of autonomous quad-rotor UAV based on double loop frame[C].Key Engineering Materials, 2011: 1421-1426.
[10] GONG X, BAI Y, ZHAO CH J, et al..Novel Hex-Rotor aircraft and its autonomous flight control system [J].Opt.Precision Eng., 2012, 20(11): 1995-2002. (in Chinese)
[11] NORDKVIST N, SANYAL A. A Lie group variational integrator for rigid body motion in SE(3) with applications to under-water vehicle dynamics[C]. Proceedings of the 49th IEEE Conference on Decision and Control, 2010: 5414-5419.
[12] LEE T, LEOK M, MCCLAMROCH N H. Geometric tracking control of a quadrotor UAV on SE(3) [C]. Proceedings of the 49th IEEE Conference on Decision and Control, 2010: 5420-5425.
[13] WANG X X, LIANG Y, PAN Q, et al..Unscented kalman filter for nonlinear systems with colored measurement noise [J].Acta Automatica Sinica, 2012, 38(6):986-998. (in Chinese)