FIELD: aviation.
SUBSTANCE: aircraft control device suitable for the independent precise indication of the space-mission vehicle (SMV) position upon incurrence off-nominal or emergency situation comprises the connected in a specific way emergency control unit, the emergency zones localization unit, the propulsion device (PD) unit, the memory unit of the phase coordinates zones, the computing unit, the unit of the independent determination of the phase coordinates of the SMV precise position at the moment of the off-nominal or emergency situation.
EFFECT: opportunity for independent precise indication of the SMV position at the moment of the off-nominal or emergency situation.
1 dwg
| Title | Year | Author | Number |
|---|---|---|---|
| DEVICE FOR CONTROLLING AN AIRCRAFT IN CASE OF EMERGENCY | 2002 |
|
RU2243587C2 |
| METHOD OF ONBOARD CONTROL IN ROCKET FLIGHT EMERGENT TERMINATION | 2011 |
|
RU2476357C2 |
| SPACE TRANSPORTATION SYSTEM ON THE BASIS OF THE LIGHT, MIDDLE AND HEAVY CLASSES ROCKETS FAMILY WITH THE SPACE ROCKETS AERIAL LAUNCH FROM THE SURFACE-EFFECT AIRBORNE SHIP BOARD AND ITS FUNCTIONING METHOD | 2014 |
|
RU2659609C2 |
| UNIVERSAL SPACE TRANSPORT SYSTEM BASED ON FAMILY OF SPACE ROCKETS OF LIGHT, MEDIUM AND HEAVY CLASSES WITH CARRIER ROCKETS LAUNCHING OVER WATER AREA OF WORLD OCEAN | 2018 |
|
RU2729912C1 |
| METHOD OF CONTROLLING ROCKET FLIGHT DURING FLIGHT TESTS | 2013 |
|
RU2549425C1 |
| METHOD OF CONTROLLING SPACE ROCKETS | 2010 |
|
RU2456217C2 |
| THRUST CONTROL DEVICE FOR THE PROPULSION SYSTEMS OF THE SOYUZ-2 AND ANGARA SPACE ROCKETS, BASED ON THE ASSESSMENT OF THE CURRENT VALUES OF THRUST DURING FLIGHT ACCORDING TO TELEMETRIC INFORMATION FOR FALLING SEPARABLE PARTS INTO A GIVEN AREA | 2022 |
|
RU2793861C1 |
| METHOD OF SAFE LAUNCHING OF ROCKET WITH MULTIENGINE FIRST STAGE | 2011 |
|
RU2481251C1 |
| METHOD OF MISSILE FLIGHT CONTROL IN FLIGHT TESTS | 1994 |
|
RU2114374C1 |
| METHOD OF DESCENT OF SPACE ROCKET BOOSTER TO TOUCHDOWN ZONE AND DEVICE FOR ITS REALIZATION | 1992 |
|
RU2043954C1 |
