Setyamartana Parman, Tiauw Hiong Go, Tuwoso
This paper proposes an integrated feed-forward input shaper for flexible spacecraft maneuvering involving coupled roll and yaw motion interactions. The shaper affects both the roll and yaw inputs, and each individual input consists of two constant amplitude pulses. The cross-contribution of the roll and yaw inputs is considered in the formulation of the residual roll and yaw oscillation constraints. The resulting shaped roll and yaw inputs are then applied to several maneuver cases of a satellite with two symmetrical flexible solar panels. The simulation results show that the proposed constraint equations to limit the residual roll and yaw oscillations are valid and correct. © 2019
Fakulti Teknologi Kejuruteraan Mekanikal dan Pembuatan, Universiti Teknikal Malaysia Melaka, Hang Tuah Jaya, Durian Tunggal, Melaka, 76100, Malaysia; Department of Aerospace, Physics and Space Sciences, Florida Institute of Technology, 150 W. University Blvd, Melbourne, 32901, FL, United States; Jurusan Teknik Mesin, Universitas Negeri Malang, Jalan Semarang 5, Malang, 65145, Indonesia
