Finite-time adaptive terminal sliding mode controller design for reusable launch vehicle in reentry phase
暂无分享,去创建一个
[1] Fang Wang,et al. Quasi-continuous high-order sliding mode controller design for reusable launch vehicles in reentry phase , 2013 .
[2] Peng Shi,et al. Active fault tolerant control design for reusable launch vehicle using adaptive sliding mode technique , 2012, J. Frankl. Inst..
[3] Dong Zhang,et al. Analysis of dynamic characteristics of the rigid body/elastic body coupling of air-breathing hypersonic vehicles , 2016 .
[4] Jie Wang,et al. Nonlinear robust control for reusable launch vehicles in reentry phase based on time-varying high order sliding mode , 2013, J. Frankl. Inst..
[5] Ji Yue-hui. Hypersonic vehicle attitude control using Terminal sliding mode control , 2013 .
[6] Qing Wang,et al. Backstepping design of missile guidance and control based on adaptive fuzzy sliding mode control , 2014 .
[7] Yuri B. Shtessel,et al. Reusable Launch Vehicle Control in Multiple Time Scale Sliding Modes , 2000 .
[8] Finite time smooth second-order sliding-mode controller design for reentry reusable launch vehicle , 2015 .
[9] S. Bhat,et al. Continuous finite-time stabilization of the translational and rotational double integrators , 1998, IEEE Trans. Autom. Control..
[10] Liu Yucha. Hypersonic vehicle attitude control based on new fast terminal sliding mode , 2015 .
[11] Xianghua Wang,et al. Partial Integrated Guidance and Control with Impact Angle Constraints , 2015 .