Opportunities search of transfer between interplanetary halo orbits in ephemeris modelYaMin Wang, PingYuan Cui, Dong Qiao · 2013

Design of optimal impulse transfers from the Sun–Earth libration point to asteroidWang, Yamin; Qiao, Dong; Cui, Pingyuan · Advances in Space Research · 2015

Opportunity options for rendezvous, flyby and sample return mission to different spectral-type asteroids for the 2015–2025Qiao Dong; Cui Pingyuan; Wang Yamin · 2012

Design and analysis of an extended mission of CE-2: From lunar orbit to Sun–Earth L2 regionQiao, Dong; Cui, Pingyuan; Wang, Yamin; Huang, Jiangchuan; Meng, Linzhi; Jie, Degang · Advances in Space Research · 2014

[IEEE 2010 International Conference on Intelligent Computing and Integrated Systems (ICISS) - Guilin, China (2010.10.22-2010.10.24)] 2010 International Conference on Intelligent Computing and Integrated Systems - Multiple gravity-assisted trajectory optimization using a hybrid methodQiao Dong, ; Cui Pingyuan, ; Wang Yamin, · 2010

Shaped Torque TechniquesSwigert, C.J. · Journal of Guidance, Control, and Dynamics · 1980

Multibody Model of an OrnithopterGrauer, Jared A.; Hubbard, James E. · Journal of Guidance, Control, and Dynamics · 2009

Predictive Missile GuidanceBest, R. A.; Norton, J. P. · Journal of Guidance, Control, and Dynamics · 2000

Optimal Deorbit GuidanceBaldwin, Morgan C.; Lu, Ping · Journal of Guidance, Control, and Dynamics · 2012

Adaptive Radome Compensation Using DitherZarchan, Paul; Gratt, Harvey · Journal of Guidance, Control, and Dynamics · 1999

Nonlinear Synergetic Optimal ControllersNusawardhana, Antonius; Zak, S. H.; Crossley, W. A. · Journal of Guidance, Control, and Dynamics · 2007

Symmetric Missile Dynamic InstabilitiesMurphy, Charles H. · Journal of Guidance, Control, and Dynamics · 1981

Missile and spacecraft coning instabilitiesPlatus, D. H. · Journal of Guidance, Control, and Dynamics · 1994