FIELD: photography. SUBSTANCE: method involves turning of aerospace vehicle through pitch angle. Vehicle is turned through pitch and yaw angles, positioned so that angular pitch, roll, and yaw velocities, and also roll angle are zero; photofilm is displaced during exposure with compensating speed calculated with due account of measurement results of vehicle orbit parameters, pitch angle, and vehicle height of flight. EFFECT: improved accuracy of image shift compensation due to considering linear velocity of ground surface at photography point during vehicle turning through pitch angle. 1 dwg
| Title | Year | Author | Number |
|---|---|---|---|
| IMAGE SHIFT COMPENSATION METHOD | 1991 |
|
RU2018894C1 |
| METHOD OF FORMING OF IMAGE FOR PHOTOGRAPHING FROM FLYING VEHICLE | 0 |
|
SU1820358A1 |
| METHOD OF COMPENSATION OF PICTURE SHIFT | 0 |
|
SU1810870A1 |
| METHOD OF DETERMINING BANKING ANGLE OF BANKING AIRCRAFT | 2013 |
|
RU2527369C1 |
| METHOD AND APPARATUS FOR CONTROLLING PILOT-NAVIGATION SYSTEM | 2010 |
|
RU2440595C1 |
| METHOD FOR DETERMINING ANGLES OF ORIENTATION OF MOVING OBJECT AND DEVICE FOR REALIZATION OF METHOD | 2004 |
|
RU2273826C2 |
| DEVICE CONTROLLING AEROPHOTOGRAPHY | 1997 |
|
RU2138780C1 |
| METHOD OF SPACECRAFT ORIENTATION AND DEVICE FOR THE METHOD REALISATION | 2016 |
|
RU2618664C1 |
| METHOD FOR INDEPENDENT DETERMINATION OF ORBIT AND ORIENTATION OF SPACECRAFT BODY IN SPACE WITHOUT PRIOR INFORMATION | 2013 |
|
RU2542599C2 |
| DEVICE FOR FORMING IMAGE AT CONICAL SCANNING | 0 |
|
SU1734233A1 |
