Add to ORKGThis paper provides a mathematical formulation and two solution algorithms of the problem of spacecraft spin axis attitude determination from noisy measurements.The two developed algorithms are compared through digital simulation and their relative merits in terms of estimation accuracy and computational requirements are discussed
© 2016 American Institute of Aeronautics and Astronautics Inc, AIAA. All rights reserved.The spin-ax...
Abstract: The paper presents the technique for determining attitude motion of a satellite ...
When quaternions are used for representing the attitude of a spinning spacecraft in an attitude esti...
This paper provides a mathematical formulation and two solution algorithms of the problem of spacecr...
This paper provides a mathematical formulation and two solution algorithms of the problem of spacecr...
This paper provides a mathematical formulation and two solution algorithms of the problem of spacecr...
A mathematical formulation of the spacecraft spin axis attitude determination problem in the form of...
A mathematical formulation of the spacecraft spin axis attitude determination problem in the form of...
Satellite attitude determination by simulation program using Monte Carlo sampling and Kalman-Schmidt...
The analysis and the FORTRAN program are presented for the determination of attitude of a spin-stabi...
Spin-stabilization offers a simple attitude control solution, specifically for micro and nanosatelli...
An attitude determination and control system for small spinning spacecraft based only on a threeaxi...
An analytical approach for spin stabilized attitude propagation is presented, considering the couple...
Abstract: The reconstruction technique is based on processing the measurements of two vect...
Presented here is a new algorithm to determine attitude using only magnetometer data under the follo...
© 2016 American Institute of Aeronautics and Astronautics Inc, AIAA. All rights reserved.The spin-ax...
Abstract: The paper presents the technique for determining attitude motion of a satellite ...
When quaternions are used for representing the attitude of a spinning spacecraft in an attitude esti...
This paper provides a mathematical formulation and two solution algorithms of the problem of spacecr...
This paper provides a mathematical formulation and two solution algorithms of the problem of spacecr...
This paper provides a mathematical formulation and two solution algorithms of the problem of spacecr...
A mathematical formulation of the spacecraft spin axis attitude determination problem in the form of...
A mathematical formulation of the spacecraft spin axis attitude determination problem in the form of...
Satellite attitude determination by simulation program using Monte Carlo sampling and Kalman-Schmidt...
The analysis and the FORTRAN program are presented for the determination of attitude of a spin-stabi...
Spin-stabilization offers a simple attitude control solution, specifically for micro and nanosatelli...
An attitude determination and control system for small spinning spacecraft based only on a threeaxi...
An analytical approach for spin stabilized attitude propagation is presented, considering the couple...
Abstract: The reconstruction technique is based on processing the measurements of two vect...
Presented here is a new algorithm to determine attitude using only magnetometer data under the follo...
© 2016 American Institute of Aeronautics and Astronautics Inc, AIAA. All rights reserved.The spin-ax...
Abstract: The paper presents the technique for determining attitude motion of a satellite ...
When quaternions are used for representing the attitude of a spinning spacecraft in an attitude esti...