Ara
Toplam kayıt 1, listelenen: 1-1
Uydu Yönelim Denetimi
(Fen Bilimleri Enstitüsü, 2013)
In this work, attitude control problem of satellites which are assumed to be as rigidbodies is addressed. Satellite attitude is represented in terms of quaternions. Due tothe nonlinear nature of satellites and in the case ...