In this dissertation, we study dynamics and attitude control problems for a multibody system in space. The key feature of this work is the systematic use of shape changes as three dimensional attitude controls. Control models are identified for a general class of multibody space systems that are controlled by thrusters, reaction wheels, and/or joint actuators. The important role of shape change in attitude maneuvers for a multibody space system is identified and shape change is recognized as a means of attitude control. Formulas that quantify three dimensional attitude changes induced by periodic shape changes, rotation of reaction wheels and nonzero angular momentum are developed. The formulas prove fundamental for development of numerous ...
Thesis: S.M., Massachusetts Institute of Technology, Department of Mechanical Engineering, 2017.Cata...
The challenging problem of controlling the attitude of satellites subject to actuator failures has b...
The challenging problem of controlling the attitude of satellites subject to actuator failures has b...
In this dissertation, we study dynamics and attitude control problems for a multibody system in spac...
. A three dimensional reorientation problem for an underactuated multibody spacecraft is studied. Fo...
In this dissertation, we develop equations of motion for a class of multibody spacecraft consisting ...
The study examines the control algorithm of a three-dimensional attitude and position of a free-floa...
This dissertation makes contributions in three areas: local equilibrium controllability analysis for...
UnrestrictedThis dissertation develops in a unified manner a new and simple approach for the modelin...
The dissertation contributes new results in three related areas: motion planning for noncatastatic n...
An attitude control strategy for maneuvers of an interconnection of planar bodies in space is develo...
Analysis of the attitude dynamics of a spacecraft is necessary for its successful operation. Recent ...
The general objective of this Ph.D. thesis is to study the dynamics and control of rigid and flexibl...
[[abstract]]This paper studies the attitude control of spacecraft hinged by a serial manipulator und...
In this paper a reorientation maneuvering strategy for an interconnection of planar rigid bodies in ...
Thesis: S.M., Massachusetts Institute of Technology, Department of Mechanical Engineering, 2017.Cata...
The challenging problem of controlling the attitude of satellites subject to actuator failures has b...
The challenging problem of controlling the attitude of satellites subject to actuator failures has b...
In this dissertation, we study dynamics and attitude control problems for a multibody system in spac...
. A three dimensional reorientation problem for an underactuated multibody spacecraft is studied. Fo...
In this dissertation, we develop equations of motion for a class of multibody spacecraft consisting ...
The study examines the control algorithm of a three-dimensional attitude and position of a free-floa...
This dissertation makes contributions in three areas: local equilibrium controllability analysis for...
UnrestrictedThis dissertation develops in a unified manner a new and simple approach for the modelin...
The dissertation contributes new results in three related areas: motion planning for noncatastatic n...
An attitude control strategy for maneuvers of an interconnection of planar bodies in space is develo...
Analysis of the attitude dynamics of a spacecraft is necessary for its successful operation. Recent ...
The general objective of this Ph.D. thesis is to study the dynamics and control of rigid and flexibl...
[[abstract]]This paper studies the attitude control of spacecraft hinged by a serial manipulator und...
In this paper a reorientation maneuvering strategy for an interconnection of planar rigid bodies in ...
Thesis: S.M., Massachusetts Institute of Technology, Department of Mechanical Engineering, 2017.Cata...
The challenging problem of controlling the attitude of satellites subject to actuator failures has b...
The challenging problem of controlling the attitude of satellites subject to actuator failures has b...