Abstract
An approach of designing of combined energy-economic control of a freeflying robotic module, used e.g. as a transport unit at its flight near by a manned orbital station is considered. The fuel consumption economy for the control of the configuration is achieved by stabilising the module's main body angular position with the help of a motion “exchange” between the module's main body's and the manipulator's links activated by their arm actuators. The control algorithms are suggested and the dynamics of the operation of all interacting subsystems module's for the combined control are investigated. A mathematical simulation was carried out taking into account the nonlinear properties of Lagrange module's equations and the nonlinear characteristics of the control subsystem's elements.
Sign-in/Register to access full text options 
Talk to us
Join us for a 30 min session where you can share your feedback and ask us any queries you have
Schedule a callDisclaimer: All third-party content on this website/platform is and will remain the property of their respective owners and is provided on "as is" basis without any warranties, express or implied. Use of third-party content does not indicate any affiliation, sponsorship with or endorsement by them. Any references to third-party content is to identify the corresponding services and shall be considered fair use under The CopyrightLaw.
