G05D1/80

Systems and methods for aircraft load alleviation

Aspects of the present disclosure generally relate to systems and methods for flight control of aircrafts driven by electric propulsion systems and in other types of vehicles. In some embodiments, a flight control system of an aircraft is disclosed, configured to receive one or more signals to control movement of the aircraft, determine at least one flight condition of the aircraft, wherein the at least one flight condition includes at least a phase of flight, calculate at least one or more loads associated with the aircraft based on the determined at least one flight condition; determine an optimized flight configuration to alleviate loads on one or more components of the aircraft based on the received one or more signals and the calculated loads, generate one or more effector commands based on the optimized flight configuration; and actuate one or more aircraft effectors based on the one or more effector commands.

Systems and methods for aircraft load alleviation

Aspects of the present disclosure generally relate to systems and methods for flight control of aircrafts driven by electric propulsion systems and in other types of vehicles. In some embodiments, a flight control system of an aircraft is disclosed, configured to receive one or more signals to control movement of the aircraft, determine at least one flight condition of the aircraft, wherein the at least one flight condition includes at least a phase of flight, calculate at least one or more loads associated with the aircraft based on the determined at least one flight condition; determine an optimized flight configuration to alleviate loads on one or more components of the aircraft based on the received one or more signals and the calculated loads, generate one or more effector commands based on the optimized flight configuration; and actuate one or more aircraft effectors based on the one or more effector commands.

DRONE SYSTEM FOR SYNTHETIC APERTURE RADAR OPERATION AND OPERATING METHOD THEREOF

A drone system for synthetic aperture radar (SAR) operation to control and operate an aerial vehicle mounted with an SAR may comprise: a flight control module configured to control a low level of the aerial vehicle; a high-level control module configured to perform communication for swarm control of the aerial vehicles, receive flight information from the flight control module, and transmit a command to the flight control module; a link module configured to link the flight control module and the high-level control module; and a data acquisition board connected to the high-level control module and configured to store a flight log from the high-level control module and radar data from a radar module provided with the SAR.

DRONE SYSTEM FOR SYNTHETIC APERTURE RADAR OPERATION AND OPERATING METHOD THEREOF

A drone system for synthetic aperture radar (SAR) operation to control and operate an aerial vehicle mounted with an SAR may comprise: a flight control module configured to control a low level of the aerial vehicle; a high-level control module configured to perform communication for swarm control of the aerial vehicles, receive flight information from the flight control module, and transmit a command to the flight control module; a link module configured to link the flight control module and the high-level control module; and a data acquisition board connected to the high-level control module and configured to store a flight log from the high-level control module and radar data from a radar module provided with the SAR.

METHOD FOR CONTROLLING A REMOTELY OPERATED VEHICLE
20250162599 · 2025-05-22 ·

Embodiments of the invention pertain to a method of controlling a remotely operated vehicle operated from a remote operation station via a communication link, the method comprising: monitoring a latency (L) of the communication link, requesting (S2) an emergency stop maneuver in response to the latency exceeding a predetermined threshold (T), and cancelling (S3) the requested emergency stop maneuver, in response to the communication link being recovered within a brake reaction time (A). Embodiments of the invention also relate to a remotely operated vehicle having a control unit configured to: monitor a latency (L) of a communication link between the vehicle and a remote operation station, request an emergency stop maneuver in response to the latency exceeding a predetermined threshold (T), and cancel the requested emergency stop maneuver, in response to the communication link being recovered within a brake reaction time period (A).

METHOD FOR CONTROLLING A REMOTELY OPERATED VEHICLE
20250162599 · 2025-05-22 ·

Embodiments of the invention pertain to a method of controlling a remotely operated vehicle operated from a remote operation station via a communication link, the method comprising: monitoring a latency (L) of the communication link, requesting (S2) an emergency stop maneuver in response to the latency exceeding a predetermined threshold (T), and cancelling (S3) the requested emergency stop maneuver, in response to the communication link being recovered within a brake reaction time (A). Embodiments of the invention also relate to a remotely operated vehicle having a control unit configured to: monitor a latency (L) of a communication link between the vehicle and a remote operation station, request an emergency stop maneuver in response to the latency exceeding a predetermined threshold (T), and cancel the requested emergency stop maneuver, in response to the communication link being recovered within a brake reaction time period (A).

DISPLAY OF 3D ILLUMINATIONS USING FLYING LIGHT SPECKS
20250165010 · 2025-05-22 ·

Present implementations can display 3D illuminations using Flying Light Specks (FLS). Each FLS can include a miniature (hundreds of micrometers) sized drone with one or more light sources to generate colors and textures with adjustable brightness. The FLS can be network enabled with a processor and local storage. Synchronized swarms of cooperating FLSs can render static and motion illumination of virtual objects in a pre-specified 3D volume, an FLS display. Present implementations can consider the limited flight time of an FLS on a fully charged battery and the duration of time to charge the FLS battery. Present implementations can accommodate failure of FLS as a norm of operation, rather than an exception. A hardware and software architectures for an FLS-display can compute flight paths of FLSs for illumination. With motion illuminations, one technique can minimize overall distance traveled by the FLSs significantly.

DISPLAY OF 3D ILLUMINATIONS USING FLYING LIGHT SPECKS
20250165010 · 2025-05-22 ·

Present implementations can display 3D illuminations using Flying Light Specks (FLS). Each FLS can include a miniature (hundreds of micrometers) sized drone with one or more light sources to generate colors and textures with adjustable brightness. The FLS can be network enabled with a processor and local storage. Synchronized swarms of cooperating FLSs can render static and motion illumination of virtual objects in a pre-specified 3D volume, an FLS display. Present implementations can consider the limited flight time of an FLS on a fully charged battery and the duration of time to charge the FLS battery. Present implementations can accommodate failure of FLS as a norm of operation, rather than an exception. A hardware and software architectures for an FLS-display can compute flight paths of FLSs for illumination. With motion illuminations, one technique can minimize overall distance traveled by the FLSs significantly.

ADAPTIVE RESPONSE FOR MARSHALING FAILURE MODES

A method of broadcasting a signal to marshal a plurality of autonomously operated vehicles including the signal broadcasted to the plurality of autonomously operated vehicles, the establishment of a secure data connection with each of the plurality of autonomously operated vehicles based on the signal, the determination of a disruption in the secure data connection to one or more vehicles of the plurality of autonomously operated vehicles, and the causation of the one or more vehicles of the plurality of autonomously operated vehicles to initiate an action based on the disruption in the secure data connection.

ADAPTIVE RESPONSE FOR MARSHALING FAILURE MODES

A method of broadcasting a signal to marshal a plurality of autonomously operated vehicles including the signal broadcasted to the plurality of autonomously operated vehicles, the establishment of a secure data connection with each of the plurality of autonomously operated vehicles based on the signal, the determination of a disruption in the secure data connection to one or more vehicles of the plurality of autonomously operated vehicles, and the causation of the one or more vehicles of the plurality of autonomously operated vehicles to initiate an action based on the disruption in the secure data connection.