[go: up one dir, main page]

Clark et al., 2010 - Google Patents

A control moment gyro for dynamic attitude control of small satellites

Clark et al., 2010

View PDF
Document ID
80670144792958319
Author
Clark C
Worrall K
Yavuzoğlu E
Publication year

External Links

Snippet

Abstract Control Moment Gyroscopes (CMGs) are not often considered for use on small satellites and, as a result few small satellite missions have implemented CMGs as on-board actuators. There are many reasons for this, but mainly this is due the complexity of the …
Continue reading at digitalcommons.usu.edu (PDF) (other versions)

Classifications

    • BPERFORMING OPERATIONS; TRANSPORTING
    • B64AIRCRAFT; AVIATION; COSMONAUTICS
    • B64GCOSMONAUTICS; VEHICLES OR EQUIPMENT THEREFOR
    • B64G1/00Cosmonautic vehicles
    • B64G1/22Parts of, or equipment specially adapted for fitting in or to, cosmonautic vehicles
    • B64G1/24Guiding or controlling apparatus, e.g. for attitude control
    • B64G1/28Guiding or controlling apparatus, e.g. for attitude control using inertia or gyro effect
    • B64G1/286Guiding or controlling apparatus, e.g. for attitude control using inertia or gyro effect using control momentum gyroscopes (CMGs)
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B64AIRCRAFT; AVIATION; COSMONAUTICS
    • B64GCOSMONAUTICS; VEHICLES OR EQUIPMENT THEREFOR
    • B64G1/00Cosmonautic vehicles
    • B64G1/22Parts of, or equipment specially adapted for fitting in or to, cosmonautic vehicles
    • B64G1/24Guiding or controlling apparatus, e.g. for attitude control
    • B64G1/28Guiding or controlling apparatus, e.g. for attitude control using inertia or gyro effect
    • B64G1/283Guiding or controlling apparatus, e.g. for attitude control using inertia or gyro effect using reaction wheels
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B64AIRCRAFT; AVIATION; COSMONAUTICS
    • B64GCOSMONAUTICS; VEHICLES OR EQUIPMENT THEREFOR
    • B64G1/00Cosmonautic vehicles
    • B64G1/22Parts of, or equipment specially adapted for fitting in or to, cosmonautic vehicles
    • B64G1/24Guiding or controlling apparatus, e.g. for attitude control
    • B64G1/36Guiding or controlling apparatus, e.g. for attitude control using sensors, e.g. sun-sensors, horizon sensors
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B64AIRCRAFT; AVIATION; COSMONAUTICS
    • B64GCOSMONAUTICS; VEHICLES OR EQUIPMENT THEREFOR
    • B64G1/00Cosmonautic vehicles
    • B64G1/22Parts of, or equipment specially adapted for fitting in or to, cosmonautic vehicles
    • B64G1/24Guiding or controlling apparatus, e.g. for attitude control
    • B64G1/26Guiding or controlling apparatus, e.g. for attitude control using jets
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B64AIRCRAFT; AVIATION; COSMONAUTICS
    • B64GCOSMONAUTICS; VEHICLES OR EQUIPMENT THEREFOR
    • B64G1/00Cosmonautic vehicles
    • B64G1/22Parts of, or equipment specially adapted for fitting in or to, cosmonautic vehicles
    • B64G1/40Arrangements or adaptations of propulsion systems
    • B64G1/402Propellant tanks; Feeding propellants
    • GPHYSICS
    • G01MEASURING; TESTING
    • G01CMEASURING DISTANCES, LEVELS OR BEARINGS; SURVEYING; NAVIGATION; GYROSCOPIC INSTRUMENTS; PHOTOGRAMMETRY OR VIDEOGRAMMETRY
    • G01C21/00Navigation; Navigational instruments not provided for in preceding groups
    • G01C21/10Navigation; Navigational instruments not provided for in preceding groups by using measurements of speed or acceleration
    • G01C21/12Navigation; Navigational instruments not provided for in preceding groups by using measurements of speed or acceleration executed aboard the object being navigated; Dead reckoning
    • G01C21/16Navigation; Navigational instruments not provided for in preceding groups by using measurements of speed or acceleration executed aboard the object being navigated; Dead reckoning by integrating acceleration or speed, i.e. inertial navigation
    • G01C21/18Stabilised platforms, e.g. by gyroscope
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B64AIRCRAFT; AVIATION; COSMONAUTICS
    • B64GCOSMONAUTICS; VEHICLES OR EQUIPMENT THEREFOR
    • B64G1/00Cosmonautic vehicles
    • B64G1/10Artificial satellites; Systems of such satellites; Interplanetary vehicles
    • B64G1/1014Navigation satellites

Similar Documents

Publication Publication Date Title
US9199746B2 (en) Attitude control system for small satellites
EP3105492B1 (en) Platform stabilization system
US6305647B1 (en) Method and apparatus for steering the attitude of a satellite
EP0849170B1 (en) System and method for reducing mechanical disturbances from energy storage flywheels
US5751078A (en) Reactionless, momentum compensated payload positioner
Beals et al. Hubble Space Telescope precision pointing control system
Verbin et al. Rapid rotational maneuvering of rigid satellites with hybrid actuators configuration
Lappas A control moment gyro (CMG) based attitude control system (ACS) for agile small satellites
KR20160125357A (en) Attitude control for agile satellite applications
Arena et al. Design, manufacturing, and ground testing of a control-moment gyro for agile microsatellites
US5261631A (en) Momentum wheel platform steering system and method
Defendini et al. Low cost CMG-based AOCS designs
Brown et al. Scissored-pair control-moment gyros: a mechanical constraint saves power
Clark et al. A control moment gyro for dynamic attitude control of small satellites
RU2702932C1 (en) Method for dynamic high-accuracy orientation and stabilization of spacecraft
Baker Feasibility and design of miniaturized Control Moment Gyroscope for a 3-axis stabilized Micro Satellite
Saberi et al. Design and analysis of gimbal thruster configurations for 3-axis satellite attitude control
Lappas et al. Design, analysis and in-orbit performance of the BILSAT-1 microsatellite twin control moment gyroscope experimental cluster
Shigeto et al. Development and Evaluation of the 1/30U Small-Sized 3 Axis Attitude Control Module, and its Application for the JEM Internal Ball Camera Robot
EP1590243A1 (en) Device for controlling the attitude of a satellite by means of gyroscopic actuators
Samuels The design and testing of a three-degree-of-freedom small satellite simulator using a linear controller with feedback linearization and trajectory generation
Li et al. Attitude control of staring-imaging satellite using Permanent Magnet momentum Exchange Sphere
Choueiri et al. Cost-Effective and Readily Manufactured Attitude Determination and Control System for NanoSatellites
You et al. Development of Modular Variable Speed Control Moment Gyro in a miniature Cube
Prassinos Design of Control Moment Gyros for Agile Small Satellites