FIELD: accident.
SUBSTANCE: system for aircraft balance control comprises sensors on body, or neck, or pilot helmet and on aircraft body, on-board flight computer configured to control rotor motors in certain manner based on sensor data.
EFFECT: higher intuitiveness, safety, convenience and clarity of flight control.
1 cl, 2 dwg
Title | Year | Author | Number |
---|---|---|---|
AIRCRAFT TAKEOFF AND LANDING AIRCRAFT SAFETY SYSTEM | 2019 |
|
RU2728451C1 |
METHOD OF EMERGENCY LANDING OF QUADCOPTER | 2017 |
|
RU2657659C1 |
CABIN PILOTED AIRCRAFT (AC) GYROSTABILIZATION SYSTEM | 2019 |
|
RU2728221C1 |
VERTICAL TAKE-OFF AND LANDING MULTIROTOR WITH IMPELLER THRUSTERS | 2020 |
|
RU2761991C2 |
DEVICE FOR CONTROL OF MANNED AIRCRAFTS OF VERTICAL TAKE-OFF AND LANDING | 2019 |
|
RU2722651C1 |
SMALL-SIZED VERTICAL TAKE-OFF/LANDING AIRCRAFT WITH AN INCREASED FLIGHT DISTANCE | 2017 |
|
RU2681464C1 |
AIRCRAFT SINGLE-WING PROPULSOR | 2019 |
|
RU2735442C1 |
MULTICOPTER FRAME (OPTIONS) | 2017 |
|
RU2657650C1 |
SYSTEM FOR INCREASING DURATION AND DISTANCE OF MULTI-COPTER FLIGHT | 2017 |
|
RU2657666C1 |
TILTROTOR CONTROL METHOD FOR VERTICAL TAKE-OFF AND LANDING | 2022 |
|
RU2795885C1 |
Authors
Dates
2020-07-28—Published
2019-10-07—Filed