[go: up one dir, main page]

Gavrilovich, 2016 - Google Patents

Development of a robotic system for CubeSat Attitude Determination and Control System ground tests

Gavrilovich, 2016

View PDF
Document ID
4450291250499340736
Author
Gavrilovich I
Publication year

External Links

Snippet

After the launch of the first artificial Earth satellite in 1957, the evolution of various technologies has fostered the miniaturization of satellites. In 1999, the development of standardized modular satellites with masses limited to a few kilograms, called CubeSats …
Continue reading at theses.hal.science (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
    • B64G1/283Guiding 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
    • B64G1/28Guiding or controlling apparatus, e.g. for attitude control using inertia or gyro effect
    • B64G1/281Spin-stabilised spacecraft
    • 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
    • B64G1/64Systems for coupling or separating cosmonautic vehicles or parts thereof, e.g. docking arrangements
    • B64G1/646Docking or rendez-vous systems
    • 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
    • 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
    • B64G1/42Arrangements or adaptations of power supply systems
    • B64G1/44Arrangements or adaptations of power supply systems using radiation, e.g. deployable solar arrays
    • 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
    • B64G1/32Guiding or controlling apparatus, e.g. for attitude control using earth's magnetic field
    • GPHYSICS
    • G09EDUCATION; CRYPTOGRAPHY; DISPLAY; ADVERTISING; SEALS
    • G09BEDUCATIONAL OR DEMONSTRATION APPLIANCES; APPLIANCES FOR TEACHING, OR COMMUNICATING WITH, THE BLIND, DEAF OR MUTE; MODELS; PLANETARIA; GLOBES; MAPS; DIAGRAMS
    • G09B9/00Simulators for teaching or training purposes
    • G09B9/02Simulators for teaching or training purposes for teaching control of vehicles or other craft
    • G09B9/52Simulators for teaching or training purposes for teaching control of vehicles or other craft for teaching control of an outer space vehicle

Similar Documents

Publication Publication Date Title
Leve et al. Spacecraft momentum control systems
Prado et al. Three-axis air-bearing based platform for small satellite attitude determination and control simulation
Underwood et al. Autonomous assembly of a reconfiguarble space telescope (aarest)–a cubesat/microsatellite based technology demonstrator
Gavrilovich Development of a robotic system for CubeSat Attitude Determination and Control System ground tests
Thomas et al. CubeSat attitude control simulator design
Schwartz The distributed spacecraft attitude control system simulator: from design concept to decentralized control
Stuchlik The wallops arc second pointer-a balloon borne fine pointing system
Paluszek ADCS-Spacecraft Attitude Determination and Control
Crowell Development and analysis of a small satellite attitude determination and control system testbed
Wolosik Advancements in the design and development of Cubesat attitude determination and control testing at the Virginia Tech space systems simulation laboratory
Cordova-Alarcon et al. Attitude Determination and Control System for the 6U CubeSat KITSUNE
Cookson Experimental investigation of spacecraft rendezvous and docking by development of a 3 degree of freedom satellite simulator testbed
Chesi Attitude control of nanosatellites using shifting masses
Belokonov et al. Problems and features of navigation and control of nanosatellites: Experience and lessons learned
Mukhayadi Efficient and high precision momentum bias attitude control for small satellite
Hennepe et al. Simulation of the attitude behaviour and available power profile of the Delfi-C3 spacecraft with application of the OpSim platform
Culton et al. Design and development of an unrestricted satellite motion simulator
Romualdez et al. The design and development of a high-resolution visible-to-near-UV telescope for balloon-borne astronomy: SuperBIT
Karataş Leo satellites: Dynamic modelling, simulations and some nonlinear attitude control techniques
Modenini et al. Nanosatellite-class dynamic attitude simulator for hands-on aerospace control education
Sorolla Bayod Study and Design of the attitude control of a cubesat 1U based on reaction wheels
Cabrales Hernandez Orbit and Attitude Control for (non-) Rotating Space-Based Telescopes Utilizing Reflectivity Control Devices
Lin et al. Attitude control for small spacecraft with sensor errors
Hernandez et al. Rotating Synthetic Aperture Space Telescope Pointing Control Demonstration and Scalability Analysis
Greene The attitude determination and control system of the generic nanosatellite bus