Author: James J. Adams
Publisher:
ISBN:
Category : Spin (Aerodynamics)
Languages : en
Pages : 28
Book Description
Simulator Study of an Active Control System for a Spinning Body
Author: James J. Adams
Publisher:
ISBN:
Category : Spin (Aerodynamics)
Languages : en
Pages : 28
Book Description
Publisher:
ISBN:
Category : Spin (Aerodynamics)
Languages : en
Pages : 28
Book Description
Study of an Active Control System for a Spinning Body
Author: James J. Adams
Publisher:
ISBN:
Category : Space vehicles
Languages : en
Pages : 34
Book Description
Publisher:
ISBN:
Category : Space vehicles
Languages : en
Pages : 34
Book Description
Simulator Study of an Active Control System for a Spinning Body
Author: James J. Adams
Publisher:
ISBN:
Category :
Languages : en
Pages : 20
Book Description
Publisher:
ISBN:
Category :
Languages : en
Pages : 20
Book Description
NASA Technical Note
Author:
Publisher:
ISBN:
Category :
Languages : en
Pages : 1094
Book Description
Publisher:
ISBN:
Category :
Languages : en
Pages : 1094
Book Description
Keywords Index to U.S. Government Technical Reports
Author:
Publisher:
ISBN:
Category : Government publications
Languages : en
Pages : 1160
Book Description
Publisher:
ISBN:
Category : Government publications
Languages : en
Pages : 1160
Book Description
Study of an Active Control System for a Spinning Body
Author: J. J. Adams
Publisher:
ISBN:
Category :
Languages : en
Pages : 1
Book Description
The mission requirements for some satellites require that they spin continuously and at the same time maintain a precise direction of the spin axis. An analog-computer study was made of anATTITUDE CONTROL SYSTEM WHICH IS SUITABLE FOR SUCH A SATELLITE. The control system provides the necessary attitude control through the use of a spinning wheel, which will provide precession torques, commanded by an automatic closed-loop servomechanism system. The sensors used in the control loop are rate gyroscopes for damping of any wobble motion and a sun seeker for attitude control. The results of the study show that the controller can eliminate the wobble motion of the satellite resulting from a rectangular pulse moment disturbance and then return the spin axis to the reference space axis. The motion is damped to half amplitude in less than one cycle of the wobble motion. The controller can also reduce the motion resulting from a step change in product of inertia both by causing the new principal axis to be steadily alined with the spin vector and by reducing the cone angle generated by the reference body axis. These methods will reduce the motion whether the satellite is a disk, sphere, or rod configuration. (Author).
Publisher:
ISBN:
Category :
Languages : en
Pages : 1
Book Description
The mission requirements for some satellites require that they spin continuously and at the same time maintain a precise direction of the spin axis. An analog-computer study was made of anATTITUDE CONTROL SYSTEM WHICH IS SUITABLE FOR SUCH A SATELLITE. The control system provides the necessary attitude control through the use of a spinning wheel, which will provide precession torques, commanded by an automatic closed-loop servomechanism system. The sensors used in the control loop are rate gyroscopes for damping of any wobble motion and a sun seeker for attitude control. The results of the study show that the controller can eliminate the wobble motion of the satellite resulting from a rectangular pulse moment disturbance and then return the spin axis to the reference space axis. The motion is damped to half amplitude in less than one cycle of the wobble motion. The controller can also reduce the motion resulting from a step change in product of inertia both by causing the new principal axis to be steadily alined with the spin vector and by reducing the cone angle generated by the reference body axis. These methods will reduce the motion whether the satellite is a disk, sphere, or rod configuration. (Author).
NASA Scientific and Technical Reports
Author: United States. National Aeronautics and Space Administration Scientific and Technical Information Division
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 260
Book Description
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 260
Book Description
A Selected Listing of NASA Scientific and Technical Reports for ...
Author:
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 450
Book Description
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 450
Book Description
Monthly Catalog of United States Government Publications
Author: United States. Superintendent of Documents
Publisher:
ISBN:
Category : Government publications
Languages : en
Pages : 1304
Book Description
Publisher:
ISBN:
Category : Government publications
Languages : en
Pages : 1304
Book Description
Scientific and Technical Aerospace Reports
Author:
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 1460
Book Description
Lists citations with abstracts for aerospace related reports obtained from world wide sources and announces documents that have recently been entered into the NASA Scientific and Technical Information Database.
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 1460
Book Description
Lists citations with abstracts for aerospace related reports obtained from world wide sources and announces documents that have recently been entered into the NASA Scientific and Technical Information Database.