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61. 发明公开

EP1797487A4 AUTONOMOUS FLIGHT FOR FLIGHT PLATFORMS 有权
标题翻译：自主飞行飞行PLATFORMS
公开(公告)号：EP1797487A4
公开(公告)日：2008-12-03
申请号：EP05787779
申请日：2005-09-26
申请人： STEADICOPTER LTD
发明人： SEGAL TUVIA
IPC分类号： B64C13/18 , B64C13/50 , B64C39/02 , B64D20060101 , G05B5/01 , G05B7/02 , G05B9/02 , G05D1/08 , G05D1/10
CPC分类号： B64C39/024 , B64C13/18 , B64C13/50 , G05D1/0858
摘要： A method and system for autonomous or semi-autonomous flight of a flight platform with flight actuators is disclosed. The system comprises a stabilization subsystem for controlling the flight actuators to maintain stabilization of the flight platform in flight and a flight control subsystem for controlling the flight actuators to implement flight control of the flight platform in flight. The two subsystems operate separately, wherein the flight control subsystem is overridden by the stabilization subsystem in an event where the flight platform exceeds a predetermined stabilization threshold until the flight platform regains stability.

62. 发明授权

EP1419088B1 BAHNFÜHRUNGS-SYSTEME FÜR EINEN FALL- ODER GLEITSCHIRM UND FLUGBAHN-PLANUNGSEINRICHTUNGEN ZUR PLANUNG DES EINSATZES ZUMINDEST EINES FALL- ODER GLEITSCHIRMS SOWIE VERFAHREN ZUR DURCHFÜHRUNG DER BAHNFÜHRUNG UND DER PLANUNG 有权
标题翻译： TRAIN SLIDE系统方面进行了跌倒或滑翔机飞行轨迹药具进行规划至少一个跌倒或滑翔伞和方法的使用实施引导与规划
公开(公告)号：EP1419088B1
公开(公告)日：2007-10-03
申请号：EP02758165.1
申请日：2002-08-23
申请人： EADS Deutschland GmbH
发明人： LOHMILLER, Winfried
IPC分类号： B64D17/00 , G05D1/00
CPC分类号： B64D1/08 , B64C13/18 , B64C31/036
摘要： The invention relates to a flight path planning device for determining path standards for at least one parachute or paraglider (5), which determines an altitude/time corridor (20, 30) as the flying range to be used by the parachute or paraglider (5), or an altitude/time line (28) as a desired standard. The limits thereof are constituted of altitude/time lines (22, 24; 31, 32) and are produced on the basis of a reference point determined by an altitude and a time coordinate. The course of the altitude/time lines is calculated from the integral of a defined sink rate (v)/time, different sink rates being associated with the altitude/time lines. The invention further relates to a path guidance system for determining control standards for controlling the parachute or paraglider.

63. 发明公开

EP1586969A1 Automatic takeoff apparatus for aircraft, automatic landing apparatus for aircraft, automatic takeoff and landing apparatus for aircraft, automatic takeoff method for aircraft, automatic landing method for aircraft and automatic takeoff and landing method for aircraft 有权
标题翻译：装置用于飞机的自动起动，进行自动着陆飞机的装置，用于自动开始和着陆的飞机，飞机自动启动方法，用于飞机和自动起飞和着陆方法用于飞机自动平层法
公开(公告)号：EP1586969A1
公开(公告)日：2005-10-19
申请号：EP05252323.0
申请日：2005-04-14
申请人： FUJI JUKOGYO KABUSHIKI KAISHA
发明人： Yamane, Akihiro
IPC分类号： G05D1/06 , B64C13/18
CPC分类号： G05D1/0653 , B64C13/18
摘要： An automatic takeoff apparatus for an aircraft (1) includes: an altitude sensor (2); an airspeed sensor (3); an attitude angle sensor (4); a direction sensor (5); a takeoff command inputting section (7); and a control device (12) for controlling a propulsion device (11) and an control surface (8,9,10) of the aircraft, wherein the control device (12) includes: a takeoff run control section for realizing a takeoff run by controlling the propulsion device to provide a maximum output and by controlling the control surface (8,9,10) to maintain the attitude angle and the traveling direction constant, in response to the takeoff command; a rotation control section for controlling the control surface (8,9,10) to rotate when the airspeed exceeds a predetermined speed; and an ascending flight control section for controlling the propulsion device and the control surface (8,9,10) to perform an ascending flight up to a target altitude with a predetermined speed maintained, when the altitude exceeds a predetermined altitude.
摘要翻译：用于飞机的自动起飞设备（1），包括：高度传感器（2）; 空速传感器（3）; 姿势角传感器（4）; 方向传感器（5）; 起飞命令输入部（7）; 和用于控制飞行器的推进装置（11）和控制面（8,9,10），worin所述控制装置（12）的控制装置（12）包括：用于实现运行起飞起飞运行控制部控制所述推进装置，以提供一个最大输出，并且通过控制所述控制表面（8,9,10），以保持姿态角和行进方向不变，响应于所述可移开的命令; 用于控制所述控制表面（8,9,10）旋转。当空速超过预定速度的旋转控制部; 并上升飞行控制部，用于控制所述推进装置与所述控制表面（8,9,10）在上升飞行到与预定速度的目标高度保持，当高度超过预定的高度来执行。

64. 发明申请

US20190200600A1 APPLICATION AND METHOD FOR CONTROLLING MOVING VEHICLE 审中-公开
公开(公告)号：US20190200600A1
公开(公告)日：2019-07-04
申请号：US16313186
申请日：2016-06-30
申请人： OPTiM Corporation
发明人： Shunji SUGAYA
IPC分类号： A01M25/00 , G05D1/00 , G05D1/10 , B64D1/18 , B64C39/02 , A01M31/00 , G06T7/00
CPC分类号： A01M25/006 , A01M7/00 , A01M31/002 , B64C13/18 , B64C39/02 , B64C39/024 , B64C2201/128 , B64D1/16 , B64D1/18 , G05D1/0038 , G05D1/101 , G06T7/0004 , G06T2207/30188
摘要： The present invention is to provide an application and a method for controlling a moving vehicle that are capable to efficiently spray a chemical. The application for controlling a moving vehicle executed on an information terminal 100 mounted on the moving vehicle 10 acquires an image taken by the information terminal 100 in flight, analyzes the acquired image, detects a pest attached to a crop based on the result of the image analysis, acquires location information of the crop to which the detected pest is attached, and controls the moving vehicle 10 to spray a disinfestant based on the acquired location information.

65. 发明申请

US20180334244A1 IN COCKPIT CONTROL OF A FIXED WING AIRCRAFT 审中-公开
公开(公告)号：US20180334244A1
公开(公告)日：2018-11-22
申请号：US15865906
申请日：2018-01-09
申请人： Sikorsky Aircraft Corporation
发明人： Igor Cherepinsky , Michael Baran , Nicholas C. Visinski
IPC分类号： B64C13/22 , B64C13/50 , B64C13/04 , B64C13/28
CPC分类号： B64C13/18 , B64C13/503
摘要： A device and method for flying an aircraft is disclosed. According to one example, the device includes a vehicle management computer configured to position a plurality of control surfaces of the aircraft to control the aircraft. The device further includes a high performance computer being configured to execute one or more high level intelligence algorithms to selectively operate the aircraft autonomously in an autonomous mode. The device further includes an actuator coupled to a piloting input, wherein the piloting input controls an aspect of the aircraft. The device further includes an actuation control unit to actuate the actuator coupled to the piloting input to move the piloting input from a first position to a second position.

66. 发明申请

US20180118370A1 VEHICLE GUIDANCE SYSTEM AND METHOD THAT USES AIR DATA FROM SURFACE-MOUNTED PRESSURE SENSORS FOR VEHICLE ORIENTATION CONTROL 审中-公开
公开(公告)号：US20180118370A1
公开(公告)日：2018-05-03
申请号：US15794080
申请日：2017-10-26
申请人： Booz Allen Hamilton Inc.
发明人： Daniel R. MILLMAN
IPC分类号： B64D43/02 , B64C13/18 , G01L19/00 , G05D1/08
CPC分类号： B64D43/02 , B64C13/18 , G01L19/0084 , G01P5/14 , G01P13/025 , G05D1/0808
摘要： A vehicle guidance system, including: sensors to detect a surface pressure distribution for a respective location of the corresponding sensor on a vehicle, respectively; and a controller to receive an initial value for a Mach number; and calculate a converged value for an angle of attack based on first surface pressure data from a first set of the sensors, and a converged sideslip angle value based on second surface pressure data from a second set of the sensors. The controller calculates a freestream dynamic pressure based on the initial Mach number, the converged angle of attack, and the converged sideslip angle value, and calculates a freestream pressure, and calculates a converged value for Mach number based on the freestream pressure and the freestream dynamic pressure. A flight control processor provides an output for adjusting an orientation of the vehicle based on the converged Mach number and the freestream pressure.

67. 发明授权

US09908616B1 Geometry-based flight control system 有权
公开(公告)号：US09908616B1
公开(公告)日：2018-03-06
申请号：US15593819
申请日：2017-05-12
申请人： Kitty Hawk Corporation
发明人： Gregory Mainland Horn , Damon Vander Lind
IPC分类号： B64C27/08 , B64D31/06 , B64C13/18 , G05D1/08 , B64D45/00 , B64C15/12
CPC分类号： B64C13/18 , B64C13/04 , B64C13/503 , B64C29/0033 , B64D31/06 , B64D2045/0085 , G05D1/0808
摘要： A geometry-based flight control system is disclosed. The geometry-based flight control system receives a set of inputs associated with a requested set of forces and moments to be applied to the aircraft and computes an optimal mix of actuators and associated actuator parameters to achieve to an extent practical the requested forces and moments. Computing the optimal mix of actuators and associated actuator parameters includes taking into consideration dynamically varying effectiveness of one or more actuators based on a dynamic state of the aircraft. For example, the dynamic state may comprise an angle of a tiltwing of the aircraft or an angle of a tilt rotor of the aircraft.

68. 发明申请

US20180056743A1 JET-PROPELLED VTOL HYBRID CAR 审中-公开
公开(公告)号：US20180056743A1
公开(公告)日：2018-03-01
申请号：US15721934
申请日：2017-10-01
申请人： Andrew H. B. Zhou , Tiger T. G. Zhou , Dylan T. X. Zhou
发明人： Andrew H. B. Zhou , Tiger T. G. Zhou , Dylan T. X. Zhou
IPC分类号： B60F5/02 , B64C37/00 , B64C29/00 , B64C3/56 , B64C5/10 , B64C7/00 , B64D25/10 , B64D27/20 , B60J5/04 , B64C13/18
CPC分类号： B60F5/02 , B60J5/0473 , B64C3/56 , B64C5/10 , B64C7/00 , B64C13/18 , B64C29/0058 , B64C29/0066 , B64C37/00 , B64D17/80 , B64D25/10 , B64D27/20
摘要： The present invention relates to a hybrid VTOL jet car comprising a light weight floatable chassis adapted for carrying a payload, a retractable tail section attached to a light weight floatable chassis at rear end adapted for stabilizing the hybrid VTOL jet car, a plurality of wheels at the bottom of the hybrid VTOL jet car, a plurality of retractable wings on the sides of light weight floatable chassis, adapted for maneuvering the hybrid VTOL jet car. Disclosed embodiments further comprising a plurality of thrust-producing engines adapted for generating the thrust required for driving the hybrid VTOL jet car on a surface as well as in the air and a plurality of parachutes attached to the hybrid VTOL jet car to safely land the hybrid VTOL jet car under emergency.

69. 发明申请

US20180039271A1 FIXED-WING DRONE, IN PARTICULAR OF THE FLYING-WING TYPE, WITH ASSISTED MANUAL PILOTING AND AUTOMATIC PILOTING 审中-公开
公开(公告)号：US20180039271A1
公开(公告)日：2018-02-08
申请号：US15672246
申请日：2017-08-08
申请人： PARROT DRONES
发明人： Ariel RIMOUX , Frédéric PIRAT
IPC分类号： G05D1/00 , G05D1/08 , G05D1/04 , B64C39/02
CPC分类号： G05D1/0088 , A63H27/12 , A63H30/04 , B64C13/18 , B64C39/024 , B64C39/10 , B64C2201/021 , B64C2201/028 , B64C2201/127 , B64C2201/141 , B64C2201/146 , G05D1/0016 , G05D1/0038 , G05D1/042 , G05D1/0653 , G05D1/0808
摘要： A drone that includes an automatic piloting system that receives internal and/or external piloting instructions, as well as data of instantaneous attitude (φ*, θ*), altitude (z*) and speed (V*) delivered by sensors. Set point calculation circuits calculate, as a function of a model of the aerodynamic behaviour of the drone in flight, roll (φ) and/or pitch (θ) set points and/or speed set points (V) and/or altitude set points (z) corresponding to the internal and/or external piloting instructions received. Correction and control circuits control the propulsion system and the drone control surface servomechanisms. A system further allows generating internally piloting instructions for autonomous flight modes such as automatic take-off or automatic landing.

70. 发明申请

US20170355467A1 Automatic flight controller, aircraft cockpit, method for operating and automatic flight controller and computer program 审中-公开
公开(公告)号：US20170355467A1
公开(公告)日：2017-12-14
申请号：US15621050
申请日：2017-06-13
申请人： Deutsches Zentrum fuer Luft- und Raumfahrt
发明人： Michael RUDOLPH , Matthias WIES
IPC分类号： B64D43/00 , G06F3/14 , B64D45/00 , B64C13/18
CPC分类号： B64D43/00 , B64C13/18 , B64D45/00 , G06F3/1423 , G09G2380/12
摘要： The invention concerns an automatic flight controller with operating elements, by means of which target settings of the automatic flight controller can be set by an operator, and with display elements for data display, wherein the display elements comprise at least two mutually separate displays that are disposed on the front, for example a front panel, of the automatic flight controller, wherein a) the at least two mutually separate displays are high resolution graphical displays and/or b) the automatic flight controller is designed to display all operating mode awareness-relevant parameters of the automatic flight controller on one or more of the at least two mutually separate displays of the automatic flight controller. The invention further concerns an aircraft cockpit with such an automatic flight controller as well as a method for operating a flight controller. The invention also concerns a computer program for carrying out the method

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