Maneuvering Spacecraft Orbit Determination Using Polynomial Representation

This paper proposed a polynomial representation-based method for orbit determination (OD) of spacecraft with the unknown maneuver. Different from the conventional maneuvering OD approaches that rely on specific orbit dynamic equation, the proposed method needs no priori information of the unknown ma...

Бүрэн тодорхойлолт

Номзүйн дэлгэрэнгүй

Үндсэн зохиолчид:	Xingyu Zhou, Tong Qin, Linzhi Meng
Формат:	Artigo
Хэл сонгох:	Inglês
Хэвлэсэн:	MDPI AG 2022-05-01
Цуврал:	Aerospace
Нөхцлүүд:	orbit determination maneuvering tracking extended Kalman filter polynomial representation
Онлайн хандалт:	https://www.mdpi.com/2226-4310/9/5/257
Шошгууд:	Шошго нэмэх Шошго байхгүй, Энэхүү баримтыг шошголох эхний хүн болох!