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Satellite Attitude Determination Planetary Landmarks

Om Satellite Attitude Determination Planetary Landmarks

Satellite Attitude Determination with Planetary Landmarks is a crucial aspect of space missions and Earth observation endeavors. It involves the precise determination of a satellite's orientation and position in space relative to identifiable features on planetary surfaces, such as landmarks or geographical points on planets or moons. The process of satellite attitude determination relies on various technologies and methodologies. Attitude sensors, such as gyroscopes and star trackers, provide essential data on the spacecraft's orientation in relation to celestial reference frames. Inertial Measurement Units (IMUs) are often used to measure the spacecraft's accelerations and rotations. Additionally, Global Navigation Satellite Systems (GNSS) can assist in the positioning of the satellite. The use of planetary landmarks plays a vital role in this determination process. By comparing the observed features on the planetary surface with known ephemeris data and image processing techniques, the satellite's orientation can be accurately estimated. Image matching algorithms and computer vision techniques are employed to identify and track these landmarks from the satellite's onboard cameras, enabling a continuous update of its position and orientation. The fusion of data from various sensors, such as the IMU and star trackers, enhances the accuracy and robustness of the satellite's attitude determination. Machine learning algorithms may be incorporated to further refine and optimize the estimation process based on past data and learned patterns. Satellite Attitude Determination with Planetary Landmarks finds applications in numerous fields, including Earth observation missions, planetary exploration, environmental monitoring, climate studies, and even space missions to other celestial bodies. Accurate knowledge of a satellite's attitude is essential for successful spacecraft navigation, instrument pointing, and data acquisition, enabling scientists and researchers to gather valuable data and images from space with precision and efficiency. Furthermore, this technique contributes to autonomous spacecraft operations, allowing the satellite to adapt and adjust its attitude in real-time, ensuring optimal performance and mission success even in dynamic and challenging space environments. As technology advances, the utilization of planetary landmarks for satellite attitude determination continues to evolve, promising increasingly accurate and reliable results for future space missions and scientific endeavors.

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  • Språk:
  • Engelsk
  • ISBN:
  • 9783155314628
  • Bindende:
  • Paperback
  • Sider:
  • 144
  • Utgitt:
  • 21. juli 2023
  • Dimensjoner:
  • 152x9x229 mm.
  • Vekt:
  • 220 g.
  Gratis frakt
Leveringstid: 2-4 uker
Forventet levering: 20. januar 2025
Utvidet returrett til 31. januar 2025
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Beskrivelse av Satellite Attitude Determination Planetary Landmarks

Satellite Attitude Determination with Planetary Landmarks is a crucial aspect of space missions and Earth observation endeavors. It involves the precise determination of a satellite's orientation and position in space relative to identifiable features on planetary surfaces, such as landmarks or geographical points on planets or moons.
The process of satellite attitude determination relies on various technologies and methodologies. Attitude sensors, such as gyroscopes and star trackers, provide essential data on the spacecraft's orientation in relation to celestial reference frames. Inertial Measurement Units (IMUs) are often used to measure the spacecraft's accelerations and rotations. Additionally, Global Navigation Satellite Systems (GNSS) can assist in the positioning of the satellite.
The use of planetary landmarks plays a vital role in this determination process. By comparing the observed features on the planetary surface with known ephemeris data and image processing techniques, the satellite's orientation can be accurately estimated. Image matching algorithms and computer vision techniques are employed to identify and track these landmarks from the satellite's onboard cameras, enabling a continuous update of its position and orientation.
The fusion of data from various sensors, such as the IMU and star trackers, enhances the accuracy and robustness of the satellite's attitude determination. Machine learning algorithms may be incorporated to further refine and optimize the estimation process based on past data and learned patterns.
Satellite Attitude Determination with Planetary Landmarks finds applications in numerous fields, including Earth observation missions, planetary exploration, environmental monitoring, climate studies, and even space missions to other celestial bodies. Accurate knowledge of a satellite's attitude is essential for successful spacecraft navigation, instrument pointing, and data acquisition, enabling scientists and researchers to gather valuable data and images from space with precision and efficiency.
Furthermore, this technique contributes to autonomous spacecraft operations, allowing the satellite to adapt and adjust its attitude in real-time, ensuring optimal performance and mission success even in dynamic and challenging space environments. As technology advances, the utilization of planetary landmarks for satellite attitude determination continues to evolve, promising increasingly accurate and reliable results for future space missions and scientific endeavors.

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