Equations of motion characterizing the three dimensional motion of a tethered satellite during the retrieval phase are studied. The mathematical model involves an arbitrary number of point masses connected by weightless cords. Motion occurs in a gravity gradient field. The formulation presented accounts for general functions describing support point motion, rate of tether retrieval, and arbitrary forces applied to the point masses. The matrix oriented program language MATLAB is used to produce an efficient vectorized formulation for computing natural frequencies and mode shapes for small oscillations about the static equilibrium configuration; and for integrating the nonlinear differential equations governing large amplitude motions. An exa...
This paper elaborates on the theory and experiment of controlling tethered spacecraft formation with...
A mathematical model is developed for studying the inplane dynamics and control of tethered two-bod...
The equations of motion of a tethered satellite system are highly nonlinear and should possess many ...
The equations of motion are developed for a perfectly flexible, inelastic tether with a satellite at...
The analysis of the rotational dynamics of the satellite was focused on the rotational amplitude inc...
Space tethered systems are attracting a lot of attention from the scientific community since they ha...
The equations of motion for a multibody tethered satellite system in three dimensional Keplerian or...
The simplest mathematical model used for the simulation of TSS motion is considered in order to revi...
Tethered satellites deployed from the Space Shuttle have been proposed for diverse applications. A f...
This research effort analyzes the fundamental dynamics governing a satellite with a gravity gradient...
Tethered Satellite Systems (TSS) has been an ongoing project around the world for many decades. This...
A relatively general mathematical model is proposed for studying the coupled attitude dynamics of sp...
A tethered satellite system consists of two or more orbiting satellites linked together by a tether ...
Simulation of two short distance crawling maneuvers of the elevator both with and without environmen...
Astronaut tethering and retrieval operations - systems analysis and design, and motion equations for...
This paper elaborates on the theory and experiment of controlling tethered spacecraft formation with...
A mathematical model is developed for studying the inplane dynamics and control of tethered two-bod...
The equations of motion of a tethered satellite system are highly nonlinear and should possess many ...
The equations of motion are developed for a perfectly flexible, inelastic tether with a satellite at...
The analysis of the rotational dynamics of the satellite was focused on the rotational amplitude inc...
Space tethered systems are attracting a lot of attention from the scientific community since they ha...
The equations of motion for a multibody tethered satellite system in three dimensional Keplerian or...
The simplest mathematical model used for the simulation of TSS motion is considered in order to revi...
Tethered satellites deployed from the Space Shuttle have been proposed for diverse applications. A f...
This research effort analyzes the fundamental dynamics governing a satellite with a gravity gradient...
Tethered Satellite Systems (TSS) has been an ongoing project around the world for many decades. This...
A relatively general mathematical model is proposed for studying the coupled attitude dynamics of sp...
A tethered satellite system consists of two or more orbiting satellites linked together by a tether ...
Simulation of two short distance crawling maneuvers of the elevator both with and without environmen...
Astronaut tethering and retrieval operations - systems analysis and design, and motion equations for...
This paper elaborates on the theory and experiment of controlling tethered spacecraft formation with...
A mathematical model is developed for studying the inplane dynamics and control of tethered two-bod...
The equations of motion of a tethered satellite system are highly nonlinear and should possess many ...