66 citations
Counting papers with at most 25 authors, so collaboration author lists do not stand in for the people here.
- Northwestern Polytechnical UniversityCN6 papers
- National University of Defense TechnologyCN5 papers
- State Key Laboratory of Aerodynamics5 papers
- Beihang UniversityCN3 papers
- Imperial College LondonGB3 papers
- Beijing Normal UniversityCN2 papers
- Chinese Academy of SciencesCN2 papers
- Hangzhou Dianzi UniversityCN2 papers
- IMDEA MaterialsES2 papers
- Stevens Institute of TechnologyUS2 papers
- Tsinghua UniversityCN2 papers
- Universidad Politécnica de MadridES2 papers
5 papers · 1 filter
Compact Formulation of the First Evolution Equation for Optimal Control Computation
Sheng Zhang, Fei Liao, Wei-Qi Qian
The first evolution equation is derived under the Variation Evolving Method (VEM) that seeks optimal solutions with the variation evolution principle. To improve the performance, i…
Computation of Optimal Control Problems with Terminal Constraint via Modified Evolution Partial Differential Equation
Sheng Zhang, Kai-Feng He, Fei Liao
The Variation Evolving Method (VEM), which seeks the optimal solutions with the variation evolution principle, is further developed to be more flexible in solving the Optimal Contr…
Aircraft trajectory control with feedback linearization for general nonlinear system
Sheng Zhang, Fei Liao, Yanqing Chen +1
The feedback linearization method is further developed for the controller design on general nonlinear systems. Through the Lyapunov stability theory, the intractable nonlinear impl…
Optimal Control Computation via Evolution Partial Differential Equation with Arbitrary Definite Conditions
Sheng Zhang, En-Mi Yong, Wei-Qi Qian
The compact Variation Evolving Method (VEM) that originates from the continuous-time dynamics stability theory seeks the optimal solutions with variation evolution principle. It is…
Robust Tracking Guidance for Zero Propellant Maneuver
Sheng Zhang, Qian Zhao, Hai-bing Huang +1
The Zero Propellant Maneuver (ZPM) maneuvers the space station by large angle, utilizing the Control Momentum Gyroscopes (CMGs) only. A robust tracking guidance strategy is propose…