45 results about "Glider" patented technology

A craft is provided with a lever that can control the power / speed of the craft and semi-automatically transition the craft in various modes of operation. This makes control of the craft somewhat similar to control of a boat, thereby bringing a maritime flight control experience to a wing-in-ground effect vehicles, hydrofoiling vessels, seagliders, and seaplanes. Further, various audio, visual, and / or haptic devices in the cockpit can provide alerts / feedback to the operator on the use of the lever and mode transitions.

An automated control system for a glider towed by a tug employs a sensor system (e.g., cameras mounted on at least one of the aircraft) to determine the relative position and velocity of the glider. A controller determines corrections to the flight characteristics of the glider in response to this data from the sensor system to maintain the glider on the surface of a limit sphere extending behind the tug with a predetermined radius based on the length of the tow cable. An interface to the flight controls of the glider maintains the desired flight characteristics of the glider provided by the controller.

Systems, devices, and methods including: an assembly configured to maintain a wing on an aircraft, the assembly comprising: a connector configured to removably connect to a first portion of the wing; and an actuator having a mechanism configured to removably engage a second portion of the wing, the second portion of the wing is configured to be moveable; wherein the actuator is configured to control the second portion of the wing.

1. Name of the product under this design: Fixed-wing glider (H1). 2. Application of this design product: for popular science education and sports equipment. 3. The key design point of this product lies in its shape. 4. The picture or photo that best illustrates the design points: Stereoscopic drawing 1.

1. The name of the designed product: toy (993C glider). 2. The use of the designed product: a flying toy. 3. The design points of the designed product: the shape of the product expressed in all views. 4. The picture or photo that best indicates the design points: perspective view 1.

The invention discloses a one-time laying system for a wave glider and a collaborative operation method of the one-time laying system, and belongs to the technical field of ocean engineering. The system comprises a wave glider and a transferring and laying device. The moving, transporting and laying device is a detachable separation support, and an upper laying support and a lower moving support are connected through a positioning pin. The laying support is provided with a bearing face matched with the ship body, four hanging rings, a supporting rod for supporting the traction machine and a floating body arranged on the middle rear portion. The method comprises the steps that the device is moved to a deck to be locked; the positioning pins are taken down, and the whole support and the glider are vertically hoisted and laid through the four slings; when the glider is immersed in water, the bracket inclines forward by using the floating body, and the glider is automatically separated; and the mother ship leaves and recycles the laying bracket. Rapid, stable and safe one-time laying of the wave glider under the complex sea condition is achieved, the risk of graded laying and umbilical cable winding are avoided, and the operation efficiency and safety are remarkably improved.

An automated control system for a glider towed by a tug employs a camera mounted on one of the aircraft to view the other (the “target”). An optical recognition system receives images from the camera and determines the relative range and bearing of the target. A controller determines corrections to the flight characteristics of the glider in response to the range and bearing data from the optical recognition system. An interface to the flight controls of the glider maintains the desired flight characteristics of the glider provided by the controller.

The present invention discloses a flight target recognition system based on a photonic neural network and a construction method. The ultrafast flight target recognition system based on a photonic neural network is designed and constructed for high-speed moving aircraft, including but not limited to airplanes, drones, helicopters, gliders, delta wings and other aircraft, as well as missiles, to achieve rapid recognition of high-speed moving targets. The present invention provides a flight target recognition system based on a photonic neural network, including an imaging and filtering module, a light field scaling and coupling module, a photonic neural network module, a mode control module, and an output light field coupling module; a construction method for a flight target recognition system, including artificial neural network design and photonic implementation of the artificial neural network; the present invention designs a photonic neural network transmission and control model based on all-optical passive components, trains for small sample learning of high-speed flying targets, builds static and dynamic target recognition systems, and realizes recognition of high-speed flying moving targets.

The application discloses a data-driven hot updraft positioning method. For a long time, unmanned aerial vehicles have been indispensable in industries such as surveillance tasks, geographic mapping and target reconnaissance. Flight endurance is a key limitation for the widespread use of unmanned aerial vehicles. However, despite researchers' efforts to modify and optimize aerodynamic shapes to reduce glider drag or replace battery reactants, there are limitations to using these methods to improve flight endurance. The present application aims to harness the energy of nature by collecting wind energy. The present application considers estimating the updraft, then estimating the position of the wind field through a sparse identification algorithm of nonlinear dynamics. The proposed SINDy-based method and its characteristics of accurately identifying the mathematical physics specification model achieve hot positioning, improve the ability to identify hot updrafts, and increase the energy of the aircraft.

The steam ejection device applied to the glider comprises a flying runway, a steam tank and an ejection system, two sliding grooves are formed in the flying runway, the ejection system is arranged below the flying runway, the ejection system comprises a sliding shuttle and two guide steel pipes arranged in parallel, and the sliding shuttle is connected with the steam tank. A guide groove is formed in the guide steel pipe, an open groove is formed in the pipe wall of the guide steel pipe, one end of the guide steel pipe is connected with the steam tank through an air pipe, a hydraulic buffer groove is formed in the other end of the guide steel pipe, a steam valve is arranged on the air pipe, and a piston is arranged at the lower end of the sliding shuttle. The piston is in sliding fit with the guide groove, a connecting plate is arranged at the upper end of the sliding shuttle, and the connecting plate penetrates through the sliding groove and is connected with a front wheel of the glider through a connecting rod. The utility model relates to the technical field of space flight and aviation.

The invention discloses a CFD-based wave glider multi-body dynamics simulation method and system, and the method comprises the steps: building an umbilical cable flexible dynamics equation through employing a concentrated mass method, and obtaining an umbilical cable flexible wave glider rigid-flexible coupling dynamics model through employing a floating body and submerged body dynamics equation as a boundary condition; the method comprises the following steps: constructing a geometric model of a floating body, a submerged body and a hydrofoil, creating a background fluid domain, carrying out regional division on the background fluid domain and the geometric model by utilizing Boolean operation, and constructing a hydrofoil-seawater bidirectional fluid-solid coupling CFD simulation model of the wave glider; building a co-simulation interface based on MATLAB-Fluent, executing time domain co-simulation and iterative updating based on the co-simulation interface, and obtaining power data in the operation process of the wave glider; according to the method, the flexible effect of the umbilical cable and the hydrofoil is introduced into the dynamic model of the wave glider, high-precision fluid-solid coupling of seawater and a structure is realized based on CFD, and the kinematics and dynamics behavior prediction precision in the operation process of the wave glider is improved.

The application discloses a wave glider motion prediction method and an optimized design parameter method based on experiments, and comprises the following steps: assigning values to the initial speed and initial position of a floating body and an underwater traction machine, obtaining umbilical cable tension and umbilical cable resistance in the initial state through an umbilical cable dynamics formula; bringing the umbilical cable tension into a floating body dynamics model to obtain the speed of the floating body; bringing the umbilical cable tension and the umbilical cable resistance into an underwater traction machine dynamics equation to obtain the speed of the underwater traction machine; respectively integrating the floating body speed and the underwater traction machine speed to obtain displacement parameters, obtaining coordinate parameters through the displacement parameters, substituting the coordinate parameters into the umbilical cable dynamics formula, and solving the umbilical cable tension and the resistance; bringing the umbilical cable tension into the floating body dynamics model, bringing the umbilical cable tension and the resistance into the underwater traction machine dynamics model, repeating the above steps, and realizing the motion prediction of the wave glider. The application can improve the precision of a simulation model.

The invention provides a wave glider high-frequency sound scattering characteristic forecasting method which comprises the following steps: dividing a wave glider into an overwater floating body ship, a connecting rod and an underwater tractor, obtaining three-dimensional geometric models of the overwater floating body ship, the connecting rod and the underwater tractor, and carrying out structure simplification; respectively establishing a grid model; the grid model is imported into Matlab, the scattering sound pressure of the grid model is obtained through a plate meta-algorithm, and then the target intensity is obtained; extracting target intensity distribution under different conditions to obtain sound scattering characteristics of the target intensity distribution; a simplified geometric model is constructed based on the actual shape of the wave glider, a high-quality triangular mesh is generated through surface discretization, and then target strength distribution under different conditions is obtained by adopting a plate element method.

The invention discloses a predetermined time adaptive control method for a wing-riding separation variant gliding aircraft, and the method specifically comprises the following steps: firstly, constructing a time scale function, and effectively avoiding the problems of unlimited increase of control quantity and singularity; secondly, designing a preset time sliding mode surface based on the time scale function; thirdly, providing a neural network parameter identification strategy, and converting a system identification problem into a parameter estimation problem so as to adapt to a flight scene with uncertain aerodynamic parameters; and finally, designing a preset time self-adaptive sliding mode controller, and realizing convergence in specified time under the condition of ensuring that the system state is not dependent on an initial condition. The adaptive gain of the controller can be dynamically adjusted according to the system environment, jitter can be inhibited, tracking errors can be reduced, and the influence caused by centralized uncertainty can be weakened; in conclusion, the control method not only realizes accurate attitude tracking, but also achieves preset time convergence characteristics irrelevant to initial conditions and control parameters, and has excellent quick responsiveness, stability and robustness.

1. The name of the design product: unmanned glider (end delivery tandem wing unmanned glider). 2. The use of the design product: used for logistics supply, can supply ground forces and emergency disaster relief supplies in various terrain environments. 3. The design points of the design product: in shape. 4. The picture or photo that best indicates the design points: perspective view.

1. The name of the design product: ocean exploration glider (sail). 2. The use of the design product: for three-dimensional detection on water, water surface, underwater. 3. The design points of the design product: in shape. 4. The picture or photo that best indicates the design points: perspective view.

The utility model provides a kind of glider and flying vehicle, it is related to aircraft technical field.Glider includes body and wing.Body is provided with containing cabin and mounting portion, containing cabin is used to contain goods or wing;Wing includes mounting shaft and two wing bodies, two wing bodies are movably arranged in mounting shaft, wing body has unfolded state and contraction state, mounting shaft is detachably arranged in mounting portion, wing is used to be contained in containing cabin in contraction state, or used to be arranged in mounting portion in contraction state or unfolded state.It can be seen that glider is reasonably configured body structure and wing form, not only improves the space utilization of glider, while enhancing its mission adaptability and delivery efficiency, and then realizes efficient, low-cost end material delivery target;In addition, it flies in the way of gliding, so it is unnecessary to install power device, further reduces the manufacturing cost of glider.

The application discloses a kind of multi-constraint terminal velocity optimal midcourse guidance methods suitable for long-range glider, including the following steps: launch platform plans the midcourse guidance trajectory of terminal velocity optimization;Launch platform extracts track point from midcourse guidance trajectory, and passes to aircraft;Aircraft generates midcourse guidance instruction according to received track point;According to midcourse guidance instruction, the flight process of aircraft is controlled.The multi-constraint terminal velocity optimal midcourse guidance method suitable for long-range glider provided by the application can meet time, angle and other terminal constraints simultaneously, and ensures that the kinetic energy loss of midcourse guidance section is minimum, and the maximum gliding distance of aircraft is enhanced.

A glider toy principally of the kick-glider genre adapted to ground launch into free flight by a user provided impact force to a rearwardly confined or linearly mobile impact surface with the main body structure configured similar to that of an aquatic water board such as the common kickboard with flat-tending surfaces contoured to impart a lift force actuated by translational velocity employing both hydrodynamic and aerodynamic principles.

1. Name of the product in this design: Scooter. 2. Purpose of this design: As a children's scooter. 3. The key design feature of this product is its shape. 4. The image or photograph that best illustrates the design's key points: 3D view 1.

A supply glider is disclosed herein. The supply glider includes a body having a first end and a second end, the body being configured to be coupled to a host aircraft, a container disposed between the first end and the second end of the body, wings coupled to the body between the first end and the second end, and stabilators coupled to the body adjacent the second end.

The application discloses a reentry gliding vehicle trajectory prediction method and relates to the technical field of reentry gliding vehicle trajectory prediction. The application constructs a time-varying parameter model set, and updates the parameter model set in real time according to the historical motion law of a target and a lateral maneuvering direction, so that the target maneuvering mutation can be effectively coped with. The application constructs different-dimension intention cost functions, comprehensively considers the distance and angle relationship among an attack target, a no-fly zone and a vehicle, constructs a distance-dimension intention cost function based on an artificial potential field method and an angle-dimension intention cost function based on a pseudo-course angle, and provides a new solution for solving the intention cost quantization of the vehicle under the existence of the no-fly zone. The application innovatively proposes to construct a multi-dimension intention fusion model, fuses different-dimension intention costs in a Bayesian inference model, avoids the inference failure problem caused by unreasonable setting of a traditional cost coefficient, and improves the universality of the intention cost function.

The invention belongs to the technical field of flight trajectory optimization, and particularly relates to a multi-algorithm trajectory optimization method for a hypersonic gliding aircraft. The method comprises the following steps: S1, setting each optimization algorithm to adopt a unified initialization parameter and a unified to-be-optimized parameter; s2, calculating an attack angle at the current flight speed according to an attack angle piecewise function; s3, calculating the height, the speed, the voyage, the heat flow, the dynamic pressure and the overload at each moment according to the motion equation of the aircraft; s4, infrared radiation energy at the terminal moment is determined according to the infrared radiation calculation model, penalty quantities caused by the height error, the voyage error and the speed error at the terminal moment are superposed, and final energy is obtained; step S5, calculating optimal parameters to be optimized by using each optimization algorithm by taking the minimum final energy as an optimization target and taking the condition that heat flow, dynamic pressure and overload are not higher than set values as constraint conditions; and S6, selecting an optimal solution from the optimization algorithms. According to the invention, the calculation efficiency and robustness are improved.

The invention provides a hydrofoil glider buoyancy compensation control method, system and device and a storage medium. The method comprises the steps of obtaining a historical water flow data sequence; inputting the historical water flow data sequence into a prediction model for prediction to obtain predicted water flow data; obtaining a lift fluctuation time sequence based on the predicted water flow data and the three-dimensional motion parameters of the hydrofoil glider; generating a compensation control instruction based on the lift fluctuation time sequence; and performing buoyancy compensation control on the hydrofoil glider based on the compensation control instruction. According to the hydrofoil glider, the key technical problem of lift fluctuation caused by water flow disturbance of the hydrofoil glider can be solved, the control difficulty of the hydrofoil glider can be fundamentally reduced, non-professionals can also easily control the hydrofoil glider, and therefore the universality of the hydrofoil glider is remarkably improved, and the application range of the hydrofoil glider is remarkably widened.

1. The name of the design product: ocean exploration glider (sail). 2. The use of the design product: for three-dimensional detection on water, water surface, underwater. 3. The design points of the design product: in shape. 4. The picture or photo that best indicates the design points: perspective view.

The invention discloses a sail configuration wave glider control system and method, and relates to the field of wave glider control, and the system comprises a sail lower computer node and a meteorological station module; the sail lower computer node is respectively connected with the folding driving module, the rotation driving module, the steering engine driving module, the state data acquisition module and the weather station module; the meteorological station module acquires meteorological data in real time and transmits the meteorological data to the sail lower computer node; the sail lower computer node receives the glider state data and the meteorological data, and determines the action state of the sail configuration wave glider according to the glider state data; calculating a target action state according to the meteorological data and the action state, and generating an automatic control instruction; and folding driving information of the folding driving module, rotation driving information of the rotation driving module and steering engine driving information of the steering engine driving module are adjusted according to the automatic control instruction. The reliability of the sail-shaped wave glider under the severe weather condition can be improved.

1. Name of the product in this design: Powered Suspension Glider. 2. Intended use of this design: for aviation sports, recreational flying, and flight experiences. 3. The key design feature of this product is its shape. 4. The image or photograph that best illustrates the design's key points: a 3D model. 5. The bottom surface of this product is a part that is not easily seen or cannot be seen during use, so the bottom view is omitted.

The invention discloses a self-adaptive sail glider course control method and system based on multi-mode perception, and relates to the technical field of path planning. The control method comprises the following steps of S1, multi-modal sensor integration and data processing, S2, real-time environment adaptation, S3, intelligent decision support and path planning, S4, adaptive course control, S5, multi-agent cooperation and feedback learning, and S6, fault detection and self-healing mechanism. By integrating various sensors and adopting a data processing technology, the complex marine environment can be comprehensively sensed, key environment indexes can be obtained in real time, the reliability of obstacle detection is improved through the multi-mode sensing capacity, it is ensured that the glider can accurately recognize potential threats under the severe sea condition, and therefore efficient obstacle avoidance path planning is achieved; and in combination with real-time weather forecast and cloud picture information, a navigation strategy can be dynamically adjusted, a navigation path is optimized, and the glider is ensured to safely and efficiently complete tasks in a complex environment.

A supply glider is disclosed herein. The supply glider includes a body having a first end and a second end, the body being configured to be coupled to a host aircraft, a container disposed between the first end and the second end of the body, wings coupled to the body between the first end and the second end, and stabilators coupled to the body adjacent the second end.

1. The name of the designed product: toy (990D glider). 2. The use of the designed product: a flying toy. 3. The design points of the designed product: the shape of the product expressed in all views. 4. The picture or photo that best indicates the design points: perspective view 1.