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自动化与信息科学期刊
SJR: 0.275 SNIP: 0.59 CiteScore™: 0.8

ISSN 打印: 1064-2315
ISSN 在线: 2163-9337

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自动化与信息科学期刊

DOI: 10.1615/JAutomatInfScien.v50.i11.60
pages 76-85

Determination of the Parameters of the Angular Motion of the Spacecraft from the Information of the Star Sensor Using the Dynamic Equation of the Solid Body Rotation in the Rodrigues–Hamilton Parameters

Nikolay V. Yefimenko
Research and Production Enterprise "Hartron-UCOM", Zaporozhye
Nataliya V. Lutsenko
Zaporozhye National Technical University, Zaporozhye

ABSTRACT

The problems of constructing the algorithms for determining the parameters of the rotational motion of a spacecraft from the information of a star sensor are considered, using the dynamic equation of the solid body rotation in the Rodrigues–Hamilton parameters. The results of modeling the work of the proposed algorithms are presented.

REFERENCES

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  2. Bar-Itzhack I.Y., Oshman Y., Attitude determination from vector observations: quaternion estimation, IEEE Transactions on Aerospace and Electronic Systems, 1985, AES-21, No. 1, 128–136.

  3. Shuster M.D., Kalman filtering of spacecraft attitude and the quest model, Journal of the Astronautical Sciences, 1990, 38, No. 3, 377–393.

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  5. Bar-Itzhack I.Y, Deutschmann J., Markley F.L., Quaternion normalization in additive EKF for spacecraft attitude determination, Proceeding of the AIAA Guidance, Navigation and Control Conf., New Orleans, LA, August, 1991, 908–916.

  6. Psiaki M.L., Theiler J., Bloch J., Ryan S., Dill R.W., Warner R.E., ALEXIS spacecraft attitude recognition with thermal/flexible motions due to launch damage, Journal of Guidance, Control, and Dynamics, 1997, 20, No. 5, 1033–1041.

  7. Kirichenko N.F., Matvienko V.T., Algorithms of asymptotic, terminal, and adaptive stabilization of rotational motions of a solid body, Problemy upravleniya i informatiki, 2003, No. 1, 5–15.

  8. Yefymenko N.V., Synthesis of control algorithms of the spacecraft spatial reorientation with the use of dynamic equations of a solid body rotational motion in Rodrigues–Hamilton parameters, Mezhdunarodnyi nauchno-tekhnicheskiy zhurnal “Problemy upravleniya i informatiki”.

  9. Yefymenko N.V., Synthesis of time optimal spatial slewing of spacecraft using dynamic equation of rigid body rotational motion at Rodrigues–Hamilton parameters, Ibid., 2017, No. 3, 109–128.


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