Application of Hamilton Principle in the control of Tethered Satellite System Pendular Motion
Journal Title: INCAS BULLETIN - Year 2018, Vol 10, Issue 2
Abstract
The control of a tethered satellite system pendular motion is done by application of Hamiltonian equation of motion on a control design method known as planar H tracking. In this case, the reference motion is considered a natural planar motion. The control of the TSS is accomplished by using the inside plane control inputs as well as the outside plane control inputs. The designed control laws are able to drive the pendular motion to a natural planar trajectory with the required characteristics. The control inputs are analyzed using their magnitude ability. The numerical simulation results for each control inputs show that the inside of plane input not only has strong magnitude, but also effectively controls the pendular motion of the tethered satellite system.
Authors and Affiliations
Paul TIROP, Zhang JINGRUI
Algorithm of probabilistic and guaranteed assessment of the current technical condition of the aircraft’s on-board systems based on the method for testing statistical hypotheses
Methods for improving the efficiency of aircraft operation by the transition to on condition operation technology are considered. Traditional methods for assessing the technical condition of the aircraft's on-board syste...
STATE OF THE ART TECHNIQUES USED FOR NOISE SOURCE IDENTIFICATION ON COMPLEX BODIES
Over the last few decades, many approaches have been undertaken in order to asses detailed noise source identification on complex bodies, i.e. aircrafts, cars, machinery. Noise source identification implies to accurately...
Aerodynamic Performance of Micro Aerial Wing Structures at Low Reynolds Number
Corrugations are folds on a surface as found on wings of dragon fly insects. Although they fly at relatively lower altitudes its wings are adapted for better aerodynamic and aero-elastic characteristics. In the present w...
Intercept Algorithm for Maneuvering Targets Based on Differential Geometry and Lyapunov Theory
Nowadays, the homing guidance is utilized in the existed and under development air defense systems (ADS) to effectively intercept the targets. The targets became smarter and capable to fly and maneuver professionally and...
Drag coefficient modelling in the context of small launcher optimisation
The purpose of this paper is to present a fast mathematical model that can be used to quickly asses the drag coefficient for generic launcher configurations. The tool developed based on this mathematical model can be use...