Add to ORKGTime optimal rest-to-rest reorientation of a rigid spacecraft with an arbitrary initial attitude and distinct principal moments of inertia is discussed. The effect of the gyroscopic coupling terms in Euler\u27s equations on the control switch times is shown. A method for recursively generating coefficients for a truncated Taylor series solution of Euler\u27s equations and the differential equations for the Euler parameter state transition matrix is shown. These solutions are used to solve for the optimal control switch times
The problem of optimal reorientation of the spacecraft orbit is considered. For solving the problem ...
We study the problem of determining time-optimal control of in-plane rendezvous transfer of spacecra...
An algorithm is proposed to solve optimal control problems arising in attitude control of a spacecra...
The nature of time optimal rotations of a rigid spacecraft with distinct principal moments of inerti...
The problem of slewing a rigid body from an arbitrary initial orientation to a desired target orient...
The nature of time optimal rotations of an axi-symmetric body is examined. In particular, the effect...
In this paper, we consider the minimum-time reorientation problem of an axi-symmetric rigid spacecra...
A Feedforward/Feedback Control Law is described for achieving near-minimum time reorientation of a r...
The problem of estimating the control switch times for minimum time rest-to-rest reorientation of a ...
Spacecraft reorientation can require propellant even when using gyroscopes since these have momentum...
The time-optimal control problem of a spacecraft equipped with reaction wheels has been studied, in ...
This article introduces a time-optimal reorientation manoeuvre controller with saturation constraint...
This work was also published as a Rice University thesis/dissertation: http://hdl.handle.net/1911/20...
The problem of optimal reorientation of the spacecraft orbit is considered. For solving the problem ...
This paper considers the problem of optimal controlling of a programmed motion of a rigid spacecr...
The problem of optimal reorientation of the spacecraft orbit is considered. For solving the problem ...
We study the problem of determining time-optimal control of in-plane rendezvous transfer of spacecra...
An algorithm is proposed to solve optimal control problems arising in attitude control of a spacecra...
The nature of time optimal rotations of a rigid spacecraft with distinct principal moments of inerti...
The problem of slewing a rigid body from an arbitrary initial orientation to a desired target orient...
The nature of time optimal rotations of an axi-symmetric body is examined. In particular, the effect...
In this paper, we consider the minimum-time reorientation problem of an axi-symmetric rigid spacecra...
A Feedforward/Feedback Control Law is described for achieving near-minimum time reorientation of a r...
The problem of estimating the control switch times for minimum time rest-to-rest reorientation of a ...
Spacecraft reorientation can require propellant even when using gyroscopes since these have momentum...
The time-optimal control problem of a spacecraft equipped with reaction wheels has been studied, in ...
This article introduces a time-optimal reorientation manoeuvre controller with saturation constraint...
This work was also published as a Rice University thesis/dissertation: http://hdl.handle.net/1911/20...
The problem of optimal reorientation of the spacecraft orbit is considered. For solving the problem ...
This paper considers the problem of optimal controlling of a programmed motion of a rigid spacecr...
The problem of optimal reorientation of the spacecraft orbit is considered. For solving the problem ...
We study the problem of determining time-optimal control of in-plane rendezvous transfer of spacecra...
An algorithm is proposed to solve optimal control problems arising in attitude control of a spacecra...