Teston et al., 2004 - Google Patents
The PROBA-1 microsatelliteTeston et al., 2004
- Document ID
- 16936682561144961576
- Author
- Teston F
- Vuilleumier P
- Hardy D
- Bernaerts D
- Publication year
- Publication venue
- Imaging Spectrometry X
External Links
Snippet
PROBA-1 is a technology demonstration mission of the European Space Agency's General Support Technology Programme. It was launched on October, 22nd, 2001 in a LEO, Sun- synchronous, 681x561 km orbit. The spacecraft mass is 94 kg, with 25 kg dedicated to …
- 229920002393 Microsatellite 0 title description 5
Classifications
-
- G—PHYSICS
- G01—MEASURING; TESTING
- G01S—RADIO DIRECTION-FINDING; RADIO NAVIGATION; DETERMINING DISTANCE OR VELOCITY BY USE OF RADIO WAVES; LOCATING OR PRESENCE-DETECTING BY USE OF THE REFLECTION OR RERADIATION OF RADIO WAVES; ANALOGOUS ARRANGEMENTS USING OTHER WAVES
- G01S19/00—Satellite radio beacon positioning systems; Determining position, velocity or attitude using signals transmitted by such systems
- G01S19/01—Satellite radio beacon positioning systems transmitting time-stamped messages, e.g. GPS [Global Positioning System], GLONASS [Global Orbiting Navigation Satellite System] or GALILEO
- G01S19/13—Receivers
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64G—COSMONAUTICS; VEHICLES OR EQUIPMENT THEREFOR
- B64G1/00—Cosmonautic vehicles
- B64G1/22—Parts of, or equipment specially adapted for fitting in or to, cosmonautic vehicles
- B64G1/24—Guiding or controlling apparatus, e.g. for attitude control
- B64G1/36—Guiding or controlling apparatus, e.g. for attitude control using sensors, e.g. sun-sensors, horizon sensors
- B64G1/363—Guiding or controlling apparatus, e.g. for attitude control using sensors, e.g. sun-sensors, horizon sensors using sun sensors
-
- G—PHYSICS
- G01—MEASURING; TESTING
- G01S—RADIO DIRECTION-FINDING; RADIO NAVIGATION; DETERMINING DISTANCE OR VELOCITY BY USE OF RADIO WAVES; LOCATING OR PRESENCE-DETECTING BY USE OF THE REFLECTION OR RERADIATION OF RADIO WAVES; ANALOGOUS ARRANGEMENTS USING OTHER WAVES
- G01S19/00—Satellite radio beacon positioning systems; Determining position, velocity or attitude using signals transmitted by such systems
- G01S19/38—Determining a navigation solution using signals transmitted by a satellite radio beacon positioning system
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64G—COSMONAUTICS; VEHICLES OR EQUIPMENT THEREFOR
- B64G1/00—Cosmonautic vehicles
- B64G1/22—Parts of, or equipment specially adapted for fitting in or to, cosmonautic vehicles
- B64G1/24—Guiding or controlling apparatus, e.g. for attitude control
- B64G1/28—Guiding or controlling apparatus, e.g. for attitude control using inertia or gyro effect
-
- G—PHYSICS
- G01—MEASURING; TESTING
- G01S—RADIO DIRECTION-FINDING; RADIO NAVIGATION; DETERMINING DISTANCE OR VELOCITY BY USE OF RADIO WAVES; LOCATING OR PRESENCE-DETECTING BY USE OF THE REFLECTION OR RERADIATION OF RADIO WAVES; ANALOGOUS ARRANGEMENTS USING OTHER WAVES
- G01S13/00—Systems using the reflection or reradiation of radio waves, e.g. radar systems; Analogous systems using reflection or reradiation of waves whose nature or wavelength is irrelevant or unspecified
- G01S13/88—Radar or analogous systems specially adapted for specific applications
- G01S13/89—Radar or analogous systems specially adapted for specific applications for mapping or imaging
- G01S13/90—Radar or analogous systems specially adapted for specific applications for mapping or imaging using synthetic aperture techniques, e.g. correcting range migration errors
- G01S13/9035—Particular SAR processing techniques not provided for elsewhere, e.g. squint mode, doppler beam-sharpening mode, spotlight mode, bistatic SAR, inverse SAR
-
- G—PHYSICS
- G01—MEASURING; TESTING
- G01C—MEASURING DISTANCES, LEVELS OR BEARINGS; SURVEYING; NAVIGATION; GYROSCOPIC INSTRUMENTS; PHOTOGRAMMETRY OR VIDEOGRAMMETRY
- G01C11/00—Photogrammetry or videogrammetry, e.g. stereogrammetry; Photographic surveying
- G01C11/02—Picture taking arrangements specially adapted for photogrammetry or photographic surveying, e.g. controlling overlapping of pictures
-
- G—PHYSICS
- G01—MEASURING; TESTING
- G01C—MEASURING DISTANCES, LEVELS OR BEARINGS; SURVEYING; NAVIGATION; GYROSCOPIC INSTRUMENTS; PHOTOGRAMMETRY OR VIDEOGRAMMETRY
- G01C21/00—Navigation; Navigational instruments not provided for in preceding groups
- G01C21/10—Navigation; Navigational instruments not provided for in preceding groups by using measurements of speed or acceleration
- G01C21/12—Navigation; Navigational instruments not provided for in preceding groups by using measurements of speed or acceleration executed aboard the object being navigated; Dead reckoning
- G01C21/16—Navigation; 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
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64G—COSMONAUTICS; VEHICLES OR EQUIPMENT THEREFOR
- B64G1/00—Cosmonautic vehicles
- B64G1/10—Artificial satellites; Systems of such satellites; Interplanetary vehicles
- B64G1/1014—Navigation satellites
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64G—COSMONAUTICS; VEHICLES OR EQUIPMENT THEREFOR
- B64G1/00—Cosmonautic vehicles
- B64G1/22—Parts of, or equipment specially adapted for fitting in or to, cosmonautic vehicles
- B64G1/42—Arrangements or adaptations of power supply systems
- B64G1/44—Arrangements or adaptations of power supply systems using radiation, e.g. deployable solar arrays
Similar Documents
Publication | Publication Date | Title |
---|---|---|
Sebestyen et al. | Low earth orbit satellite design | |
Graf et al. | The Mars reconnaissance orbiter mission | |
Di Tana et al. | ArgoMoon: There is a Nano-Eyewitness on the SLS | |
Roncoli et al. | Mission design overview for the Mars exploration rover mission | |
Slavinskis et al. | Nanospacecraft fleet for multi-asteroid touring with electric solar wind sails | |
Speretta et al. | LUMIO: achieving autonomous operations for Lunar exploration with a CubeSat | |
Johnston et al. | The Mars reconnaissance orbiter mission | |
Sorensen et al. | The Clementine mission—A 10-year perspective | |
Teston et al. | The PROBA-1 microsatellite | |
Smrekar et al. | Venus Origins Explorer (VOX) concept: A proposed new frontiers mission | |
Teston et al. | Proba, an ESA technology demonstration mission, results after 3 years in orbit | |
Lee et al. | Mars Reconnaissance Orbiter design approach for high-resolution surface imaging | |
Bernaerts et al. | Proba (Project for on-board autonomy) | |
Martin-Mur et al. | Using optical communications links for deep-space navigation | |
Dinaol | Analysis of ETRSS-1 on-orbit performance and anomaly management | |
Amoroso et al. | Italian Cubesats for Moon and Asteroid imaging | |
Wloszek et al. | FTS CubeSat constellation providing 3D winds | |
Iwata et al. | Advanced Land Observing Satellite (ALOS): Development and On-Orbit Status | |
Cawthorne et al. | Launching 2009: the nigeriasat-2 mission–high-performance earth observation with a small satellite | |
Lund | US Magellan Spacecraft that Explored Venus 1980–2020 | |
Dandumont | From mission analysis to systems engineering of the OUFTI-Next nanosatellite | |
Hardhienata et al. | Technical Aspects and Attitude Control Strategy of LAPAN-TUBSAT Micro Satellite | |
Rose et al. | NASA’s Cyclone Global Navigation Satellite System (CYGNSS) Mission–Temporal Resolution of a Constellation Enabled by Micro-Satellite Technology | |
Adams et al. | Precision control, knowledge and orbit determination on a small spacecraft bus: The orbview-4 attitutde control system | |
Mowle et al. | The Landsat-6 satellite: an overview |