FIELD: aviation.
SUBSTANCE: group of inventions refers to a method and system for preventing collisions of a manned aircraft with the earth's surface, as well as a multifunctional maneuverable aircraft. To prevent collisions determine the parameters of the position and motion of the aircraft, the maximum height of the terrain in the monitoring zone, calculate the loss of height when the automatic withdrawal is activated, form several auto-trajectory trajectories, select the trajectory in a certain way and carry out an automatic retraction when they reach a certain height. System contains an air speed meter, a navigation system, control computer, automatic control system and remote control system, indicating and signaling means, a height-adjusting device connected in a certain way. Multifunctional maneuverable aircraft contains a comprehensive control system with automatic and remote control systems, a system for measuring air-speed parameters and a system of limiting signals, an information-control system with a computer system and means of indication, signaling and control systems, a complex of flight-navigation equipment with navigation sensors and terrain-keeping means, an interlocking lock-in for automatic withdrawal.
EFFECT: it is ensured that the aircraft is maneuvered at an extremely low altitude.
10 cl, 3 dwg, 1 tbl
Title | Year | Author | Number |
---|---|---|---|
METHOD AND SYSTEM FOR PREVENTION OF AIRCRAFT COLLISION WITH TERRAIN RELIEF | 2007 |
|
RU2368954C2 |
METHOD OF PREVENTION OF COLLISION OF FLYING VEHICLE WITH GROUND AND DEVICE FUNCTIONING ON BASIS OF THIS METHOD | 2006 |
|
RU2301456C1 |
COLLISION AVOIDANCE SYSTEM FOR FLIGHT TESTS | 1996 |
|
RU2134911C1 |
METHOD FOR PREVENTION OF THREAT OF AIRCRAFT COLLISION WITH OBSTACLES OF UNDERLYING SURFACE | 2007 |
|
RU2356099C1 |
METHOD AND SYSTEM FOR FORMATION OF ASSESSMENT OF AIRCRAFT FLIGHT ABSOLUTE HEIGHT, MULTIFUNCTIONAL MANEUVERING PLANE EQUIPPED THEREWITH | 2017 |
|
RU2671613C1 |
METHOD OF PREVENTING COLLISION OF AIRPLANES AND HELICOPTERS WITH TERRAIN FEATURES AND DEVICE BASED ON SAID METHOD | 2008 |
|
RU2376645C1 |
SYSTEM FOR PREVENTING COLLISION OF AIRCRAFT WITH GROUND | 2005 |
|
RU2271039C1 |
INTELLIGENT SYSTEM OF CREW SUPPORT | 2013 |
|
RU2541902C2 |
SMART CREW SUPPORT SYSTEM | 2015 |
|
RU2598130C1 |
CONTROL SYSTEM IN LONGITUDINAL CHANNEL OF MANNED AND UNMANNED AIRCRAFTS IN MODE OF CREEPING FROM DANGEROUS HEIGHT AT WORK ON GROUND OBJECTS | 2016 |
|
RU2644048C2 |
Authors
Dates
2018-08-15—Published
2017-08-08—Filed