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Mission planning is an effective support and important guarantee for agile satellites to implement earth observation missions. According to traditional mission planning methods by which the mission and attitude are independently planned, the observation efficiency of agile satellites cannot be fully utilized. This paper considers the cooperative planning of mission and attitude, and establishes a...
To solve the real-time orbit determination for impulse maneuver satellite, this paper proposes a strong tracking cubature Kalman filter (STCKF) algorithm. This algorithm uses the equivalent representation of strong tracking filter (STF) to calculate suboptimal fading factor so as to real-timely adjust the gain matrix online. In this way, residual error series are forced to be mutually orthogonalized,...
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