Abstract
The principal objective of the paper at hand is to introduce the idea of a new optimal spacecraft attitude estimation algorithm. The proposed optimal attitude estimation algorithm depends mainly on the optimal fusion of the outputs of spacecraft attitude determination and/or estimation algorithms. This proposed optimal fusion algorithm is able to generate attitude estimates with better standard deviation than the determination and/or estimation algorithms alone. The proposed optimal attitude estimation algorithm is not standalone because it needs at least another hardware measurement sensor in addition to determination and/or estimation algorithms.
Sign-in/Register to access full text options 
Free) 
Talk to us
Join us for a 30 min session where you can share your feedback and ask us any queries you have
Schedule a call
