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Study of an Active Control System for a Spinning Body

Study of an Active Control System for a Spinning Body PDF Author: James J. Adams
Publisher:
ISBN:
Category : Space vehicles
Languages : en
Pages : 34

Book Description


Study of an Active Control System for a Spinning Body

Study of an Active Control System for a Spinning Body PDF Author: James J. Adams
Publisher:
ISBN:
Category : Space vehicles
Languages : en
Pages : 34

Book Description


Simulator Study of an Active Control System for a Spinning Body

Simulator Study of an Active Control System for a Spinning Body PDF 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

Simulator Study of an Active Control System for a Spinning Body PDF Author: James J. Adams
Publisher:
ISBN:
Category :
Languages : en
Pages : 20

Book Description


Study of an Active Control System for a Spinning Body

Study of an Active Control System for a Spinning Body PDF 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).

NASA Technical Note

NASA Technical Note PDF Author:
Publisher:
ISBN:
Category :
Languages : en
Pages : 282

Book Description


Scientific and Technical Aerospace Reports

Scientific and Technical Aerospace Reports PDF Author:
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 1278

Book Description


A Selected Listing of NASA Scientific and Technical Reports for ...

A Selected Listing of NASA Scientific and Technical Reports for ... PDF Author:
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 450

Book Description


NASA Scientific and Technical Reports

NASA Scientific and Technical Reports PDF Author: United States. National Aeronautics and Space Administration Scientific and Technical Information Division
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 260

Book Description


Keywords Index to U.S. Government Technical Reports

Keywords Index to U.S. Government Technical Reports PDF Author:
Publisher:
ISBN:
Category : Government publications
Languages : en
Pages : 1160

Book Description


Bibliography Related to Human Factors System Program

Bibliography Related to Human Factors System Program PDF Author: Richard J. Potocko
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 252

Book Description