[d-6] Attitude determination

[2023-ｄ-22] EQUULEUS' In-Space Least Squares Thrust Vector Estimation with Non-linear Observation Model

*Vinicius Ferreira Nery¹, Shunichiro Nomura¹, Ryohei Takahashi¹, Toshihiro Suzuki¹, Hirotaka Sekine¹, Yosuke Kawabata¹, Ryu Funase^1,2 (1. The University of Tokyo, 2. JAXA)

キーワード：In-space Thrust Vector Estimation, Delta-V, Attitude Control, Deep Space Cubesat, EQUULEUS