Szczegóły

Tytuł artykułu

Single-Frame Attitude Determination Methods for Nanosatellites

Tytuł czasopisma

Metrology and Measurement Systems

Rocznik

2017

Wolumin

vol. 24

Numer

No 2

Autorzy

Wydział PAN

Nauki Techniczne

Wydawca

Polish Academy of Sciences Committee on Metrology and Scientific Instrumentation

Data

2017

Identyfikator

ISSN 0860-8229

Referencje

Hajiyev (2002), Increase of accuracy of the small satellite attitude determination using redundancy techniques, Acta Astronautica, 50, 673. ; Shuster (1981), Three - Axis Attitude Determination from Vector Observations of Guidance and Control, Journal, 4, 70. ; Shuster (1993), A Survey of Attitude Representations The of the Astronautical, Journal Sciences, 41. ; Markley (1993), Attitude Determination Using Vector Observations : a Fast Optimal Matrix Algorithm Jouranl of Astronaut, Sci, 41, 261. ; Vallado (2001), Fundamentals of Astrodynamics and Applications Springer Media, Science Business. ; Zanardi (2016), Numerical and analytical approach for the spin - stabilized satellite attitude propagation, Comp Appl Math, 1. ; Bar (1996), REQUEST A Recursive QUEST Algorithm for Sequential Attitude Determination of Guidance , Control , and, Journal Dynamics, 19, 1034. ; Wahba (1965), Problem Least Squares Estimate of Satellite Attitude, Siam Review, 65, 409. ; Markley (1991), Attitude Determination And Parameter - Estimation Using Vector Observations Application of the Astronautical, Journal Sciences, 39, 367. ; Garcia (2015), Unscented Kalman filter for spacecraft attitude estimation using modified Rodrigues parameters and real data, Comp Appl Math, 1. ; Vinther (2011), Inexpensive Cubesat Attitude Estimation Using Quaternions And Unscented Kalman Filtering Control in, Automatic Aerospace, 4. ; Hajiyev (2016), Nontraditional Approach to Satellite Attitude Estimation of Control Systems and Robotics, International Journal, 19. ; Shuster (2004), Deterministic Three - Axis Attitude Determination of Astronaut, Journal Sci, 52, 405. ; Habib (2013), A comparative study of spacecraft attitude determination and estimation algorithms ( a cost - benefit approach ) and, Aerospace Science Technology, 26, 211. ; Markley (2000), Quaternion attitude estimation using vector observations of the Astronautical, Journal Sciences, 48, 359.

DOI

10.1515/mms-2017-0023

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