B64D1/00

Multicopter-assisted system and method for launching and retrieving a fixed-wing aircraft

The present disclosure provides various embodiments of a multicopter-assisted launch and retrieval system generally including: (1) a multi-rotor modular multicopter attachable to (and detachable from) a fixed-wing aircraft to facilitate launch of the fixed-wing aircraft into wing-borne flight; (2) a storage and launch system usable to store the modular multicopter and to facilitate launch of the fixed-wing aircraft into wing-borne flight; and (3) an anchor system usable (along with the multicopter and a flexible capture member) to retrieve the fixed-wing aircraft from wing-borne flight.

Multicopter-assisted system and method for launching and retrieving a fixed-wing aircraft

The present disclosure provides various embodiments of a multicopter-assisted launch and retrieval system generally including: (1) a multi-rotor modular multicopter attachable to (and detachable from) a fixed-wing aircraft to facilitate launch of the fixed-wing aircraft into wing-borne flight; (2) a storage and launch system usable to store the modular multicopter and to facilitate launch of the fixed-wing aircraft into wing-borne flight; and (3) an anchor system usable (along with the multicopter and a flexible capture member) to retrieve the fixed-wing aircraft from wing-borne flight.

Multicopter-assisted system and method for launching and retrieving a fixed-wing aircraft

The present disclosure provides various embodiments of a multicopter-assisted launch and retrieval system generally including: (1) a multi-rotor modular multicopter attachable to (and detachable from) a fixed-wing aircraft to facilitate launch of the fixed-wing aircraft into wing-borne flight; (2) a storage and launch system usable to store the modular multicopter and to facilitate launch of the fixed-wing aircraft into wing-borne flight; and (3) an anchor system usable (along with the multicopter and a flexible capture member) to retrieve the fixed-wing aircraft from wing-borne flight.

Unmanned aerial vehicle delivery systems

Certain embodiments of the present application relate to a method for releasing a parcel from an unmanned aerial vehicle (UAV). The parcel is engaged with a hook attached to a line suspended from the UAV. The method includes lowering the hook such that the parcel is at least partially supported by a target surface, thereby performing an attempt to release the parcel from the hook, performing at least one iteration of an iterative procedure. The iterative procedure includes raising the hook, and determining whether the line remains loaded. The iterative procedure further includes lowering the hook an additional time in response to a determination that the line remains loaded, thereby performing an additional attempt to release the parcel from the hook. The iterative procedure further includes performing an additional iteration of the iterative procedure in response to the number of attempts failing to satisfy a threshold number of attempts.

SCISSOR ARM FOR UNMANNED ROBOTIC SYSTEM
20190389080 · 2019-12-26 ·

The present invention recites a scissor arm for an unmanned robotic system such as a UAV, also known as a drone. This arm would typically be installed on the underside of a UAV with hover capability. The arm is designed to simultaneously vertically lower and horizontally extend a payload, permitting a person to interact with the payload without risk of injury by the UAV's propellers. This arm is practical for applications such as a routine police traffic stop, wherein an officer can safely remain in their vehicle and interact with the driver via a drone equipped with communication equipment and such an arm. The drone's arm can present the driver with a box for gathering documents from the driver without risk of injuring the driver or damaging the driver's vehicle. This is accomplished by two inventive L-shaped trusses that offset the arm's payload horizontally as the arm is extended downward.

SCISSOR ARM FOR UNMANNED ROBOTIC SYSTEM
20190389080 · 2019-12-26 ·

The present invention recites a scissor arm for an unmanned robotic system such as a UAV, also known as a drone. This arm would typically be installed on the underside of a UAV with hover capability. The arm is designed to simultaneously vertically lower and horizontally extend a payload, permitting a person to interact with the payload without risk of injury by the UAV's propellers. This arm is practical for applications such as a routine police traffic stop, wherein an officer can safely remain in their vehicle and interact with the driver via a drone equipped with communication equipment and such an arm. The drone's arm can present the driver with a box for gathering documents from the driver without risk of injuring the driver or damaging the driver's vehicle. This is accomplished by two inventive L-shaped trusses that offset the arm's payload horizontally as the arm is extended downward.

MISSION PLANNER FOR THE AERIAL RELEASE OF MOSQUITOES
20240074407 · 2024-03-07 · ·

A method and system for preparing a distribution program for insects comprises obtaining distribution data of a wild population of insects; obtaining distribution parameters including distribution resolution levels of at least one available distribution vehicle; generating a population density map at a resolution level consistent with the distribution resolution level of the vehicle; generating a release map by modifying the population density map in accordance with the distribution parameters; and generating a path using the release map, the path defining dosages of insects to be released at respective locations along the path.

MISSION PLANNER FOR THE AERIAL RELEASE OF MOSQUITOES
20240074407 · 2024-03-07 · ·

A method and system for preparing a distribution program for insects comprises obtaining distribution data of a wild population of insects; obtaining distribution parameters including distribution resolution levels of at least one available distribution vehicle; generating a population density map at a resolution level consistent with the distribution resolution level of the vehicle; generating a release map by modifying the population density map in accordance with the distribution parameters; and generating a path using the release map, the path defining dosages of insects to be released at respective locations along the path.

MULTICOPTER WITH SELF-ADJUSTING ROTORS
20240045446 · 2024-02-08 ·

During a vertical landing state, it is decided whether to switch from the vertical landing state to a self adjusting state. The VTOL vehicle includes the flight controller, the rotor, and a fuselage where the rotor is coupled to the fuselage via a vertical connector. If it is so decided, there is a switch from the vertical landing state to the self adjusting state. During the self adjusting state, a control signal for a rotor is generated where the control signal causes: (1) the rotor to rotate during the self adjusting state and (2) the VTOL vehicle to remain in a fixed position during the self adjusting state, in response to the control signal, and independent of docking infrastructure. During a rotors off state, a rotor off control signal is generated for the rotor that causes the rotor to turn off.

MULTICOPTER WITH SELF-ADJUSTING ROTORS
20240045446 · 2024-02-08 ·

During a vertical landing state, it is decided whether to switch from the vertical landing state to a self adjusting state. The VTOL vehicle includes the flight controller, the rotor, and a fuselage where the rotor is coupled to the fuselage via a vertical connector. If it is so decided, there is a switch from the vertical landing state to the self adjusting state. During the self adjusting state, a control signal for a rotor is generated where the control signal causes: (1) the rotor to rotate during the self adjusting state and (2) the VTOL vehicle to remain in a fixed position during the self adjusting state, in response to the control signal, and independent of docking infrastructure. During a rotors off state, a rotor off control signal is generated for the rotor that causes the rotor to turn off.