• Chinese Journal of Lasers
  • Vol. 49, Issue 17, 1704003 (2022)
Liang Hu1、2、3、*, Huixian Duan1、3, Haodong Pei1、3、**, Dianqi Sun1、2、3, and An Shu1、3
Author Affiliations
  • 1Key Laboratory of Intelligent Infrared Perception, Chinese Academy of Sciences, Shanghai 200083, China
  • 2University of Chinese Academy of Sciences, Beijing 100049, China
  • 3Shanghai Institute of Technical Physics, Chinese Academy of Sciences, Shanghai 200083, China
  • show less
    DOI: 10.3788/CJL202249.1704003 Cite this Article Set citation alerts
    Liang Hu, Huixian Duan, Haodong Pei, Dianqi Sun, An Shu. Binocular Vision Position and Attitude Measurement for Key Features of Non-Cooperative Spacecraft[J]. Chinese Journal of Lasers, 2022, 49(17): 1704003 Copy Citation Text show less
    Converging binocular stereo vision measurement model
    Fig. 1. Converging binocular stereo vision measurement model
    Result images of the candidate ellipse of arc segment combination. (a) Arc-support segment method; (b) improved method
    Fig. 2. Result images of the candidate ellipse of arc segment combination. (a) Arc-support segment method; (b) improved method
    Result image of the outer docking ring of non-cooperative target
    Fig. 3. Result image of the outer docking ring of non-cooperative target
    Result images of heat shield reticles detection. (a) Proposed method; (b) Hough transform
    Fig. 4. Result images of heat shield reticles detection. (a) Proposed method; (b) Hough transform
    Schematic diagram of the coordinate system. (a) Measurement coordinate system and camera coordinate system; (b) target coordinate system
    Fig. 5. Schematic diagram of the coordinate system. (a) Measurement coordinate system and camera coordinate system; (b) target coordinate system
    Schematic diagram of position and attitude measurement process
    Fig. 6. Schematic diagram of position and attitude measurement process
    Absolute and relative position and attitude during the approach. (a) Absolute position; (b) absolute angle; (c) relative position; (d) relative angle
    Fig. 7. Absolute and relative position and attitude during the approach. (a) Absolute position; (b) absolute angle; (c) relative position; (d) relative angle
    MethodNumber of candidate ellipsesVerification time /sEllipse extraction time /s
    Arc-support segment320.61200.9530
    Improved120.07200.2430
    Table 1. Analysis of the results of two ellipse detection methods
    No.x /cmy /cmz /cmθx/(°)θy/(°)θz/(°)
    1402.467-7.6669.317-42.079-4.387-0.002
    2402.557-7.7119.329-44.189-4.4390.245
    3402.539-7.7579.357-46.181-4.4290.600
    4402.506-7.7969.386-48.096-4.4430.904
    5402.655-7.8599.423-50.116-4.4571.204
    6402.560-7.8909.450-52.261-4.4271.463
    7402.634-7.9409.493-54.289-4.4151.737
    8402.828-8.0029.515-56.374-4.3431.989
    9402.852-8.0399.618-58.292-4.2442.228
    Table 2. Position and attitude measurement results when the satellite model rotates around the X axis
    No.x /cmy /cmz /cmθx/(°)θy/(°)θz/(°)
    1400.005-6.84210.015-167.6474.373-1.906
    2399.276-6.84410.066-167.8194.105-0.429
    3398.506-6.78710.062-167.6293.3570.876
    4398.086-6.76110.088-167.3663.1432.160
    5398.025-6.81810.089-166.7202.8833.436
    6397.737-6.79610.125-166.4042.6674.599
    7397.432-6.78710.141-166.1092.4515.747
    8397.081-6.75610.181-165.7542.2546.898
    9396.699-6.69710.226-166.1002.0547.929
    10396.249-6.64710.282-166.1751.9179.047
    Table 3. Position and attitude measurement results when the satellite model rotates around the Z axis
    No.x /cmy /cmz /cmθx/(°)θy/(°)θz/(°)
    1399.424-6.89110.124-167.7793.292-2.318
    2399.672-6.83810.169-167.4692.026-2.475
    3399.834-6.82110.223-167.2830.956-2.602
    4399.855-6.82610.282-167.521-0.366-2.532
    5399.868-6.83310.349-167.407-1.521-2.515
    6399.811-6.84310.424-167.648-2.515-2.399
    7399.769-6.85810.508-167.335-3.795-2.249
    8399.705-6.87610.589-167.637-5.048-2.181
    9399.647-6.88610.675-167.512-6.221-1.903
    Table 4. Position and attitude measurement results when the satellite model rotates around the Y axis
    Liang Hu, Huixian Duan, Haodong Pei, Dianqi Sun, An Shu. Binocular Vision Position and Attitude Measurement for Key Features of Non-Cooperative Spacecraft[J]. Chinese Journal of Lasers, 2022, 49(17): 1704003
    Download Citation