Quaternion Interpolation Under the Angular Velocity Constraint

被引:1
|
作者
Gokce, Murat [1 ]
Gulmammadov, Farid [2 ]
Soken, Halil Ersin [3 ]
Sozen, Semsettin Numan [1 ]
机构
[1] TUBITAK Space Technol Res Inst, Attitude & Orbit Control Syst, Ankara, Turkiye
[2] Plans S Satellite & Space Technol, Attitude & Orbit Control Syst, Ankara, Turkiye
[3] Middle East Tech Univ, Aerosp Engn Dept, Ankara, Turkiye
关键词
quaternion interpolation; attitude determination; satellite rotation; euler angles;
D O I
10.1109/RAST57548.2023.10197985
中图分类号
V [航空、航天];
学科分类号
08 ; 0825 ;
摘要
In this paper we present a novel approach to interpolate the attitude. Quaternions are used to define the attitude for space vehicles and in some missions such as Earth imaging, considering the periodically incoming quaternion data, if an image is taken between two periods, obtaining the quaternion data of the relevant moment can only be found by interpolating the previous quaternion information. Unlike the current quaternion interpolation methods in the literature, we implement the spline method under the angular velocity constraint in order to interpolate the quaternions from the derived Euler angles so that to obtain more accurate quaternions information in the desired time interval.
引用
收藏
页数:6
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