Dynamics-based attitude determination using the global positioning system

被引:10
作者
Chun, C [1 ]
Park, FC [1 ]
机构
[1] Seoul Natl Univ, Sch Mech & Aerosp Engn, Seoul 151742, South Korea
关键词
D O I
10.2514/2.4767
中图分类号
V [航空、航天];
学科分类号
08 ; 0825 ;
摘要
We present an algorithm for attitude determination using Global Positioning System (GPS) phase difference measurements. The problem is formulated as an optimization problem on the group of rotation matrices subject to the system's kinematic and dynamic equations of motion. We first formulate an objective function ir:hose update at each time step requires the integration of the dynamic equations and employs a forgetting factor to weight the history of accumulated CPS measurements. In the event that angular velocity measurements are not available, a cubic spline interpolation algorithm on the rotation group is used to estimate the angular, velocity from the available attitude measurements. A geometric version of Newton's algorithm on the rotation group is also employed for the optimization, together with a method for rapidly calculating a suboptimal solution to be used as the initial point in the iteration. Simulation results comparing the performance of the proposed algorithm with those that neglect the dynamics are given.
引用
收藏
页码:466 / 473
页数:8
相关论文
共 20 条
[1]  
Astrom K. J., 1995, ADAPTIVE CONTROL, P42
[2]   Attitude estimation algorithms for spinning satellites using global positioning system phase data [J].
Axelrad, P ;
Behre, PC .
JOURNAL OF GUIDANCE CONTROL AND DYNAMICS, 1997, 20 (01) :164-169
[3]   Spacecraft attitude estimation using the global positioning system: Methodology and results for RADCAL [J].
Axelrad, P ;
Ward, LM .
JOURNAL OF GUIDANCE CONTROL AND DYNAMICS, 1996, 19 (06) :1201-1209
[4]   Algorithms for attitude determination using the global positioning system [J].
Bar-Itzhack, I ;
Montgomery, PY ;
Garrick, JC .
JOURNAL OF GUIDANCE CONTROL AND DYNAMICS, 1998, 21 (06) :846-852
[5]  
Cohen CE., 1996, Reston, P519
[6]   Predictive filtering for attitude estimation without rate sensors [J].
Crassidis, JL ;
Markley, FL .
JOURNAL OF GUIDANCE CONTROL AND DYNAMICS, 1997, 20 (03) :522-527
[7]   Minimum model error approach for attitude estimation [J].
Crassidis, JL ;
Markley, FL .
JOURNAL OF GUIDANCE CONTROL AND DYNAMICS, 1997, 20 (06) :1241-1247
[8]   Efficient and optimal attitude determination using recursive global positioning system signal operations [J].
Crassidis, JL ;
Lightsey, EG ;
Markley, FL .
JOURNAL OF GUIDANCE CONTROL AND DYNAMICS, 1999, 22 (02) :193-201
[9]   New algorithm for attitude determination using global positioning system signals [J].
Crassidis, JL ;
Markley, FL .
JOURNAL OF GUIDANCE CONTROL AND DYNAMICS, 1997, 20 (05) :891-896
[10]   SPACECRAFT ATTITUDE-CONTROL AND STABILIZATION - APPLICATIONS OF GEOMETRIC CONTROL-THEORY TO RIGID BODY MODELS [J].
CROUCH, PE .
IEEE TRANSACTIONS ON AUTOMATIC CONTROL, 1984, 29 (04) :321-331