Fig. 1. Schematic diagram of the experimental system. (a) Geometric relationship of the on-orbit imaging; (b) top view

Fig. 2. Relationship between target rotation speed and satellite maneuvering angular speed along flight direction

Fig. 3. Schematic of the ground experiment system

Fig. 4. Static imageing of the target. (a) Design drawing of the target; (b) physical photo corresponding to the dotted frame

Fig. 5. Relationship between dynamic MTF and light intensity

Fig. 6. Dynamic imaging of the target. (a) Change of dynamic MTF with the angular velocity of the target; (b) dynamic image with 128 levels and a rotation speed of 800 (°)/s

Fig. 7. Result of the dynamic imaging. (a) Variation curve of the integration time ; (b) partial images of the target dynamic imaging