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ANALYSIS AND JUSTIFICATION OF RELIABILITY REQUIREMENTS FOR PERSPECTIVE SPACE VEHICLES
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| AIRBORNE AND GROUND EQUIPMENT CONTROL COMPLEXES |
| V.A. Ovsyannikov, Y.V. Ovsyannikov, V.L. Filippov |
ON THE POSSIBILITIES OF USING THERMAL IMAGERS TO DETECT OBSTACLES THAT IMPEDE FLYING HELICOPTERS
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| SECURITY IN AUTOMATIC AND MANUAL MODES FLIGHT |
| L.E. Mistrov, E.M. Shepovalov |
ANALYSIS AND JUSTIFICATION OF RELIABILITY REQUIREMENTS FOR PERSPECTIVE SPACE VEHICLES
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| S.V. Bezdenezhnykh, T.A. Zharova, E.B. Khapov, Z.A. Val |
HELICOPTER LANDING IN CASE OF PARTIAL FAILURE OF THE TAIL ROTOR
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| CONTROL, STABILIZING, NAVIGATION, ORIENTATION AND AIMING SYSTEMS |
| A.V. Molodenkov, Ya.G. Sapunkov, T.V. Molodenkova |
ALGORITHM OF THE OPTIMAL REORIENTATION WITH A COMBINED OBJECTIVE FUNCTIONAL FOR AN AXIALLY SYMMETRIC SPACECRAFT IN THE CLASS OF CONICAL MOTIONS
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