A5047168670- Dynamics and Control of Mechanical Systems
- Adaptive Control of Nonlinear Systems
- Astro and Planetary Science
- Spacecraft Dynamics and Control
- Space Satellite Systems and Control
- Vibration Control and Rheological Fluids
- Stellar, planetary, and galactic studies
- Scheduling and Optimization Algorithms
- Structural Analysis and Optimization
- Regional Development and Environment
- Distributed and Parallel Computing Systems
- Stability and Control of Uncertain Systems
- Industrial Automation and Control Systems
Harbin Institute of Technology
2017-2023
Nanjing University of Aeronautics and Astronautics
2017
Heilongjiang Institute of Technology
2017
Jiangsu Normal University
2010
The problem of flexible spacecraft attitude tracking control with guaranteeing the prescribed performance is investigated. First, Lagrangian model derived. Then, a model-free law proposed, in which information and appendage not required. proposed able to guarantee transient steady-state behavior for both angular velocity errors presence bounded external disturbances. stability resulting closed-loop system guaranteed by Lyapunov approach. Two special forms are subsequently obtained....
In this paper, a trajectory optimization method for generating smooth and approximate time-optimal attitude maneuver trajectories of flexible spacecraft is proposed. Smooth highly desirable spacecraft, since vibration appendices can be suppressed. order to obtain trajectory, novel objective function composed two terms developed in the problem optimization: first term proportional total time other one integral squared control torque derivatives. This latter ensures that generated smooth. The...
A time suboptimal method for on-orbit rapid attitude maneuver control of agile spacecraft with angular velocity constraint is proposed, which can generate torque command real-time application. Spacecraft time-optimal slew has been studied by many researchers, and most the interest focused on formulating resolving optimization problem in proper ways. Pseudospectral method, among existing methods, feasible to figure out preferred solution satisfying precision, possesses values practical...
No AccessEngineering NotesDistributed Optimization Method for Spacecraft Attitude Control and Vibration SuppressionYabo Hu, Franco Bernelli-Zazzera Yunhai GengYabo HuHarbin Institute of Technology, 150001 Harbin, People's Republic China, Bernelli-ZazzeraPolytechnic University Milan, 20156 Italy GengHarbin ChinaPublished Online:1 Feb 2023https://doi.org/10.2514/1.G007097SectionsRead Now ToolsAdd to favoritesDownload citationTrack citations About References [1] Singhose W. E., Banerjee A. K....