1 Ocak 2017 Dergi makalesi Açık Erişim

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

Citation Style Language JSON

{
  "DOI": "10.1515/mms-2017-0023", 
  "abstract": "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.", 
  "author": [
    {
      "family": "Cilden Guler", 
      "given": " Demet"
    }, 
    {
      "family": "Conguroglu", 
      "given": " Ece S."
    }, 
    {
      "family": "Hajiyev", 
      "given": " Chingiz"
    }
  ], 
  "container_title": "METROLOGY AND MEASUREMENT SYSTEMS", 
  "id": "48259", 
  "issue": "2", 
  "issued": {
    "date-parts": [
      [
        2017, 
        1, 
        1
      ]
    ]
  }, 
  "page": "313-324", 
  "title": "SINGLE-FRAME ATTITUDE DETERMINATION METHODS FOR NANOSATELLITES", 
  "type": "article-journal", 
  "volume": "24"
}