Skyryse, Inc.

Mark Groden

Mitch Adler

Nur Harell

Christopher Charles Ward

Gonzalo Javier Rey

Jonathan R Reeves

Justin Mark Ryan

Zeke Robert Markshausen

Christopher Camilo Cole

Christopher Ryan Smith

Daniel James Stillion

A landing site selection system selects landing sites for unplanned landings for small aircraft. The landing site selection system may generate a landing site database comprising parameters for landing sites. The landing sites may be any location where an aircraft may potentially land. The landing site selection system may monitor aircraft conditions and determine that an unplanned landing may be desirable. The landing site selection system may select potential landing sites based on the aircraft conditions and the landing site parameters. The landing site selection system may display landing site parameters for the selected landing sites to a pilot to allow the pilot to select a landing site. The landing site selection may provide navigation instructions or autonomously navigate the aircraft to the landing site.

Unplanned landing site selection for aircraft

Mechanical controller

Embodiments relate to an aircraft control router for an aircraft. The aircraft control router may include a command processing module, sensor validation module, aircraft state estimation module, and control laws module. The command processing module may be configured to generate aircraft trajectory values based on received aircraft control inputs. The sensor validation module may be configured to validate sensor signals generated by sensors of the aircraft. The aircraft state estimation module may be configured to determine an estimated aircraft state of the aircraft based on the validated sensor signals. The control laws module may be configured to generate actuator commands for actuators of the aircraft to adjust control surfaces of the aircraft, where the generated actuator commands are based on aircraft trajectory values, validated sensor signals, and an estimated aircraft state. The aircraft control router may transmit the generated actuator commands to actuators of the aircraft.

Vehicle control router

Electronic display console and mechanical controller configuration

Controlling aircraft traffic in an aerial network is described. A controller system identifies a departure site, an arrival site, a departure time interval, and an arrival time interval. Based on the on the departure site, the arrival site, and the departure time interval, the controller system generates a spatiotemporal region. A spatiotemporal region defines a three-dimensional perimeter that moves in time along a flightpath from the departure site to the arrival site. An aircraft is assigned to the spatiotemporal region and instructed to remain within perimeter of the spatiotemporal region as the aircraft travels from the departure site to the arrival site. The controller system monitors locations of the aircraft over time relative to the perimeter of the spatiotemporal region. If the aircraft deviates from the spatiotemporal region, the controller may transmit control instructions to the aircraft to return to the spatiotemporal region.

Aerial vehicle network traffic control

A method, preferably including: sampling inputs, determining aircraft conditions, and/or acting based on the aircraft conditions. A method, preferably including: sampling inputs, determining input reliability, determining guidance, and/or controlling aircraft operation. A method, preferably including: operating the vehicle, planning for contingencies, detecting undesired flight conditions, and/or reacting to undesired flight conditions. A system, preferably an aircraft such as a rotorcraft, configured to implement the method.

Situational awareness, vehicle control, and/or contingency planning for aircraft actuator failure

A method for providing medical services to a patient, including: receiving a medical service request associated with a patient location; selecting an aircraft, located at an initial location, from a plurality of aircraft based on the patient location and the initial location; determining a flight plan for flying the aircraft to a region containing the patient location; at a sensor of the aircraft, sampling a first set of flight data; at a processor of the aircraft, autonomously controlling the aircraft to fly based on the flight plan and the set of flight data; selecting a landing location within the region; and landing the aircraft at the landing location, including: sampling a set of landing location data; determining a safety status of the landing location based on the set of landing location data; outputting a landing warning observable at the landing location; at the sensor, sampling a second set of flight data; and in response to determining the safety status and outputting the landing warning, autonomously controlling the aircraft to land at the landing location based on the second set of flight data.

Vehicle system and method for providing services

A system and a method are disclosed for a vehicle control and interface system configured to facilitate control of different vehicles through universal mechanisms. The vehicle control and interface system can be integrated with different types of vehicles (e.g., rotorcraft, fixed-wing aircraft, motor vehicles, watercraft, etc.) in order to facilitate operation of the different vehicles using universal vehicle control inputs. In particular, the vehicle control and interface system converts universal vehicle control inputs describing a requested trajectory of a vehicle received from one or more universal vehicle control interfaces into commands for specific actuators of the vehicle configured to adjust a current trajectory of the vehicle to the requested trajectory. In order to convert the universal vehicle control inputs to actuator commands the vehicle control and interface system processes the universal vehicle control inputs using a universal vehicle control router.

Vehicle control and interface system

A safety system for an aerial vehicle, preferably including: a ballistic subsystem, preferably including one or more rockets operable to adjust motion of the aerial vehicle and a mounting unit that couples the ballistic subsystem to the aerial vehicle; and/or a deployable parachute subsystem. An aerial vehicle, preferably including a safety system. A method for aerial vehicle operation, preferably including activating a safety system.

Growing community of inventors

San Francisco, CA, United States of America

Mark Groden