Vladimir S. Syromiatnikov Spacecraft Docing Devices deom SSI

Figure 7.7. Hybrid complex test unit. Principal scheme of the control, computing, executive, and recording equipment. 1. control panel of system of thermal regulation; 2. system of thermal regulation; 3. hydraulic supply system; 4. control panel of hydraulic system; 5. command to control tracking drives; 6. main computer, conversion of forces and momenta, computation of the reactions of the control system, conversion of coordinates, integration of equations of motion, formation of control commands; 7. central control panel of test unit, control of modes, communications, indication, emergency shut-off; 8. from force sensors; 9. executive test unit; 10. controlling computer, preparation and verification, control of subsystems, control before contact, data processing; 11. system of emergency cessation of testing,, detection of flaws, automatic monitoring, emergency shut-off; 12. measurement and recording system; 13. control panel of docking assemblies. Tn the initial stage of displacement of the platform the computer controls the drive so that at the calculated moment of first contact the assemblies occupy the

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