Open Access
MATEC Web of Conferences
Volume 31, 2015
2015 7th International Conference on Mechanical and Electronics Engineering (ICMEE 2015)
Article Number 02004
Number of page(s) 5
Section Mechanical power engineering
Published online 23 November 2015
  1. Luo X, Li J. Fuzzy dynamic characteristic model based attitude control of hypersonic vehicle in gliding phase. Sci China Inf Sci, 2011; 54: 448–459. [CrossRef]
  2. Fan M, Cao W, Fang X J. Prediction of hypersonic boundary layer transition with variable specific heat on plane flow. Sci China-Phys Mech Astron, 2011; 54: 2064–2070. [CrossRef]
  3. Liu Xiaodong, Zhang Yu, Huang Wanwei, Wang Jianmin. Research of a fuzzy global sliding mode control scheme: A stability control scheme for anti-aircraft missile with swing nozzle thrust vector control. Proc I MechE, Part G: J Aerospace Engineering 2015; 229: 554–561. [CrossRef]
  4. Schaefermeyer MR. Aerodynamic thrust vectoring for attitude control of a vertically thrusting jet engine. USA, MSc, Utah State University, 2011.
  5. Yeh FK. Sliding-mode-based contour-following controller for guidance and autopilot systems of launch vehicles. Proc I MechE, Part G: J Aerospace Engineering 2013; 227: 285–302. [CrossRef]
  6. Vinayagam AK and Sinha NK. An assessment of thrust vector concepts for twin-engine airplane. Proc I MechE, Part G: J Aerospace Engineering 2013; 228: 960–979. [CrossRef]
  7. Yonghua Wang, Benwei Li, Keyi. Jiang Research on Take-Off Performance of an Aircraft Installing Thrust-Vectoring Nozzles. Journal of Naval Aeronautical and Astronautical University 2008; 23(6),626–644.
  8. Saghafi F and Banazadeh A. Investigation on the flight characteristics of a conceptual fluidic thrust-vectored aerial tail-sitter. Proc I MechE, Part G: J Aerospace Engineering 2007; 229: 27–37.