1 Ocak 2017 Dergi makalesi Açık Erişim

Cilden Guler, Demet; Conguroglu, Ece S.; Hajiyev, Chingiz

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        "affiliation": "Istanbul Tech Univ, Fac Aeronaut & Astronaut, TR-34469 Istanbul, Turkey", 
        "name": "Cilden Guler, Demet"
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      {
        "affiliation": "Istanbul Tech Univ, Fac Aeronaut & Astronaut, TR-34469 Istanbul, Turkey", 
        "name": "Conguroglu, Ece S."
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      {
        "affiliation": "Istanbul Tech Univ, Fac Aeronaut & Astronaut, TR-34469 Istanbul, Turkey", 
        "name": "Hajiyev, Chingiz"
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    "description": "Single-frame methods of determining the attitude of a nanosatellite are compared in this study. The methods selected for comparison are: Single Value Decomposition (SVD), q method, Quaternion ESTimator (QUEST), Fast Optimal Attitude Matrix (FOAM) - all solving optimally the Wahba's problem, and the algebraic method using only two vector measurements. For proper comparison, two sensors are chosen for the vector observations on-board: magnetometer and Sun sensors. Covariance results obtained as a result of using those methods have a critical importance for a non-traditional attitude estimation approach; therefore, the variance calculations are also presented. The examined methods are compared with respect to their root mean square (RMS) error and variance results. Also, some recommendations are given.", 
    "doi": "10.1515/mms-2017-0023", 
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    "journal": {
      "issue": "2", 
      "pages": "313-324", 
      "title": "METROLOGY AND MEASUREMENT SYSTEMS", 
      "volume": "24"
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    "license": {
      "id": "cc-by"
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    "publication_date": "2017-01-01", 
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    "title": "SINGLE-FRAME ATTITUDE DETERMINATION METHODS FOR NANOSATELLITES"
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