FIELD: rocket technology; aviation.
SUBSTANCE: aircraft equipment is designed to evade aircraft from damage by anti-aircraft missiles and air-to-air missiles. Serves to assist the pilot in performing an overload maneuver, where vision, consciousness or the cardiac arrest is lost. System has a tunable dual-mode autopilot, its first mode ensures the retention of the course and the height of the aircraft when the wheel is released by having a push-button on the steering wheel, and its the second mode provides an anti-missile maneuver, for example, a "dead loop" maneuver in the plane specified by the pilot before releasing the helm or before the voice command is given to activate the second autopilot mode.
EFFECT: system increases the possible overload of the aircraft while maneuvering.
9 cl
| Title | Year | Author | Number |
|---|---|---|---|
| ANTIGRAVITY SUIT (VERSIONS) | 2011 |
|
RU2452665C1 |
| ANTI-AIRCRAFT MISSILE - 2 | 2017 |
|
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| METHOD AND DEVICE FOR CHECKING AND CONTROLLING PILOT FUNCTIONAL CONDITION IN FLIGHT | 1999 |
|
RU2150886C1 |
| ANTI-OVERLOAD DEVICE (VERSIONS) WITH DEVICE OF CONTROL THEREFROM (VERSIONS) | 2008 |
|
RU2400403C2 |
| ATTACK AIRCRAFT (VERSIONS) | 2016 |
|
RU2623638C1 |
| ATTACK AIRCRAFT - 2 (OPTIONS) | 2017 |
|
RU2655588C1 |
| MISSILE AND METHOD FOR ITS OPERATING | 2014 |
|
RU2590760C2 |
| DUAL-MODE SEEKER HEAD | 2017 |
|
RU2661504C1 |
| METHOD OF CHECK AND CONTROL OF FUNCTIONAL AND PHYSIOLOGICAL CONDITION OF PILOT IN FLIGHT AND DEVICE FOR REALIZATION OF THIS METHOD | 2000 |
|
RU2170953C1 |
| AIRCRAFT VARIABLE MANUAL CONTROL (VERSIONS) | 2012 |
|
RU2505456C1 |
