34results about How to "Short flight distance" patented technology

The invention discloses an unmanned plane flight control system. The unmanned plane flight control system comprises a main controller, an execution mechanism, a communication device and a ground station device. The master control system comprises a data collection module, a data processing module and a communication module. The data collection module is used for collecting measurement signals of various sensors and uploading the measurement signals to the data processing module. The data processing module can perform management and control on various flight modes and on an execution mechanismin the unmanned plane flight. The execution mechanism comprises a motor electric regulation device and a spraying device. The ground station device can perform track programming and can perform formation on multiple unmanned planes to carry out cooperated programming of multiple unmanned planes. The master controller realizes unmanned plane terrain simulation flight control, highly reliable faulttolerance control and autonomous obstacle avoidance control.

An object of the present invention is to provide a golf ball having an improved controllability and shot feeling while maintaining a flight distance on driver shots. The present invention provides a golf ball having a core, an intermediate layer disposed around the core, and a cover disposed around the intermediate layer, wherein the core has a center and an envelope layer disposed around the center, and has a specific hardness distribution, and the intermediate layer is formed from an intermediate layer composition comprising, as a resin component, (A) a modified polyester elastomer and (B) a binary ionomer resin, and having a flexural modulus ranging from 150 MPa to 450 MPa, a maximum loss factor (tan δ) between −20° C. and 0° C. of 0.08 or less, a repulsive modulus of 55% or more, and a slab hardness ranging from 60 to 90 in JIS-hardness.

A golf ball includes a spherical core and a cover covering the spherical core, wherein the cover is formed from a polyurethane composition containing a polyurethane elastomer as a resin component, the polyurethane composition has a shear loss modulus G″ of more than 5.03×106 Pa and 1.17×108 Pa or less when measured in a shear mode using a dynamic viscoelasticity measuring apparatus at the conditions of the temperature of 0° C., and the oscillation frequency of 10 Hz, the golf ball has a hardness distribution that R2 of a linear approximate curve determined by a least-squares method is 0.95 or more, when plotting center hardness (JIS-C) of the spherical core, hardness (JIS-C) measured at intervals of 2.5 mm from the center of the spherical core, surface hardness (JIS-C) of the spherical core, and slab hardness (JIS-C) of the cover versus distances from the center of the spherical core.

The present invention provides a golf ball comprising a spherical core and at least one cover layer covering the spherical core, wherein the cover is formed from a polyurethane composition containing a polyurethane elastomer as a resin component, the polyurethane composition satisfying properties of rebound resilience of 54% or more and a shear loss modulus G″ of 5.03×106 Pa or less when measured in a shear mode using a dynamic viscoelasticity measuring apparatus at the conditions of the temperature of 0° C., and the oscillation frequency of 10 Hz, and the spherical core has a hardness distribution that R2 of a linear approximate curve determined by a least-squares method is 0.95 or more, when plotting JIS-C hardness measured at a center, a surface and at intervals of 2.5 mm from the center of the spherical core, versus distances from the center of the spherical core.

The invention discloses an automatic unmanned plane express delivery shortest path program method. The address information of each to-be-delivered express is scanned through scanning equipment, all target sites of a present delivery task are determined, and the shortest path starting from an express distribution center, passing by all the target sites and finally returning back to the express distribution center is programmed. An initialization algorithm is firstly provided, a population including a series of molecules is generated, and each molecule represents a feasible path satisfying the delivery task; four corresponding chemical reaction sub algorithms are further provided, including a decomposition algorithm, a synthesis algorithm, a local search algorithm and a greedy search algorithm, iteration is carried out according to relevant rules, the molecule population is made to realize continuous evolution till iteration termination conditions are satisfied, a molecule of the population having the smallest potential energy is found out, and the optimal path is programmed. The method is advantaged in that on the condition that the delivery task of all the target express sites is accomplished, the total flight path of the unmanned plane is the shortest, the total consumption time is the shortest, consumption energy is effectively reduced, and express delivery efficiency is improved.

An object of the present invention is to provide a golf ball which travels a great distance on the driver shots and stops quickly on the green on the approach shots. The present invention is directed to a golf ball material having a shear loss modulus G″ of 2.11×107 Pa or less, and a ratio (E″ / G″) of a tensile loss modulus E″ to the shear loss modulus G″ of 1.78 or more, when measuring the shear loss modulus G″ in a shear mode and the tensile loss modulus E″ in a tensile mode at conditions of a temperature of 0° C., oscillation frequency of 10 Hz using a dynamic viscoelasticity measuring apparatus.

The invention discloses an air route planning method for multi-unmanned aerial vehicle target positioning, which is used for solving the technical problem of poor practicability of an existing unmanned aerial vehicle air route planning method. According to the technical scheme, the method comprises the steps of firstly, enabling a navigation system of an unmanned aerial vehicle to obtain the position information of the unmanned aerial vehicle, and searching to obtain the approximate position of a ground fixed target; and obtaining the flight speed v, the maximum roll angle and the radius R ofa trajectory circle flying around the fixed target of the unmanned aerial vehicle as the initialization parameters. Under the condition that the initial positions of the multiple unmanned aerial vehicles are random, it can be guaranteed that the multiple unmanned aerial vehicles can rapidly reach the space above the target, and an equidistant formation configuration on a trajectory circle is rapidly formed. According to the method, the information needed by planning is little, the engineering implementation is easy, the calculated amount is very small, and the planning speed is high; the formed planned road section only has a straight line section and a curved line section, the flight distance is as short as possible, the flight time is as short as possible, and the practicability is good.

An object of the present invention is to provide a golf ball intermediate layer resin composition with an excellent resilience and fluidity. Another object of the present invention is to provide a golf ball intermediate layer resin composition with a high hardness and durability. Yet another object of the present invention is to provide a golf ball traveling a great distance with an ionomer intermediate layer. The present invention provides a golf ball intermediate layer resin composition comprising, (A) an ionomer resin consisting of a metal ion-neutralized product of a binary copolymer composed of an olefin and an α,β-unsaturated carboxylic acid having 3 to 8 carbon atoms; (B) a binary copolymer composed of an olefin and an α,β-unsaturated carboxylic acid having 3 to 8 carbon atoms, and (C) a zinc compound, wherein a content ratio ((A) / (B)) of (A) component to (B) component ranges from 50 / 50 to 80 / 20 in a mass ratio and a content of (C) component ranges from 0.1 part to 20 parts with respect to 100 parts by mass of a sum of (A) component and (B) component, and the golf ball intermediate layer resin composition has a melt flow rate (190° C., 2.16 kg) of 15 g / 10 min or more.

An object of the present invention is to provide a golf ball cover resin composition containing an ionomer resin with an excellent resilience and fluidity. Another object of the present invention is to provide a golf ball using an ionomer resin for a cover, with an excellent shot feeling, durability and resilience. The present invention provides a golf ball cover resin composition comprising (A) an ionomer resin consisting of a metal ion-neutralized product of a ternary copolymer composed of an olefin, an α,β-unsaturated carboxylic acid having 3 to 8 carbon atoms and an α,β-unsaturated carboxylic acid ester; (B) a binary copolymer composed of an olefin and an α,β-unsaturated carboxylic acid having 3 to 8 carbon atoms and / or a ternary copolymer composed of an olefin, an α,β-unsaturated carboxylic acid having 3 to 8 carbon atoms and an α,β-unsaturated carboxylic acid ester, and (C) a zinc compound, wherein a content ratio ((A) / (B)) of (A) component to (B) component ranges from 50 / 50 to 80 / 20 in a mass ratio and a content of (C) component ranges from 0.1 part to 20 parts with respect to 100 parts by mass of a sum of (A) component and (B) component, and the golf ball cover resin composition has a melt flow rate (190° C., 2.16 kg) of 5 g / 10 min or more.

The invention discloses a sabot separation device of a high-speed air cannon. The sabot separation device comprises a vacuum cavity, a deflating hole is formed in the vacuum cavity, and a thin film isarranged on the deflating hole. The separation device has small influence to the speed and attitude of an emitted projectile body and is convenient to install and maintain

The invention provides a course reversal method and device of an unmanned aerial vehicle, and relates to the field of unmanned aerial vehicles. The problem that an unmanned aerial vehicle has a relatively large risk in a flight process of flying to a standby landing point. The specific technical scheme is as follows: acquiring a target route, wherein the target route is a flight route of a currently executed flight task of the unmanned aerial vehicle; acquiring a standby landing point list, wherein the standby landing point list comprises at least one standby landing point; matching a course reversal point of the unmanned aerial vehicle with the at least one standby landing point according to the target route and a preset algorithm; determining a landing point of the unmanned aerial vehicle from the at least one standby landing point according to a matching result; and controlling the unmanned aerial vehicle to fly to the landing point along the target route. The unmanned aerial vehicle course reversal method and device provided by the invention are applied to course reversal of unmanned aerial vehicles.

An object of the present invention is to provide a golf ball which travels a great distance on the driver shots and stops quickly on the green on the approach shots. The present invention is directed to a golf ball material having a shear loss modulus G″ of 2.11×107 Pa or less, and a ratio (E″ / G″) of a tensile loss modulus E″ to the shear loss modulus G″ of 1.78 or more, when measuring the shear loss modulus G″ in a shear mode and the tensile loss modulus E″ in a tensile mode at conditions of a temperature of 0° C., oscillation frequency of 10 Hz using a dynamic viscoelasticity measuring apparatus.

An object of the present invention is to provide a golf ball having an improved controllability and shot feeling while maintaining a flight distance on driver shots. The present invention provides a golf ball having a core, an intermediate layer disposed around the core, and a cover disposed around the intermediate layer, wherein the core has a center and an envelope layer disposed around the center, and has a specific hardness distribution, and the intermediate layer is formed from an intermediate layer composition comprising, as a resin component, (A) a modified polyester elastomer and (B) a binary ionomer resin, and having a flexural modulus ranging from 150 MPa to 450 MPa, a maximum loss factor (tan δ) between −20° C. and 0° C. of 0.08 or less, a repulsive modulus of 55% or more, and a slab hardness ranging from 60 to 90 in JIS-hardness.

An object of the present invention is to provide a golf ball cover resin composition containing an ionomer resin with an excellent resilience and fluidity. Another object of the present invention is to provide a golf ball using an ionomer resin for a cover, with an excellent shot feeling, durability and resilience. The present invention provides a golf ball cover resin composition comprising (A) an ionomer resin consisting of a metal ion-neutralized product of a ternary copolymer composed of an olefin, an α,β-unsaturated carboxylic acid having 3 to 8 carbon atoms and an α,β-unsaturated carboxylic acid ester; (B) a binary copolymer composed of an olefin and an α,β-unsaturated carboxylic acid having 3 to 8 carbon atoms and / or a ternary copolymer composed of an olefin, an α,β-unsaturated carboxylic acid having 3 to 8 carbon atoms and an α,β-unsaturated carboxylic acid ester, and (C) a zinc compound, wherein a content ratio ((A) / (B)) of (A) component to (B) component ranges from 50 / 50 to 80 / 20 in a mass ratio and a content of (C) component ranges from 0.1 part to 20 parts with respect to 100 parts by mass of a sum of (A) component and (B) component, and the golf ball cover resin composition has a melt flow rate (190° C., 2.16 kg) of 5 g / 10 min or more.

An object of the present invention is to provide a golf ball resin composition containing an ionomer resin with an excellent resilience and fluidity. Another object of the present invention is to provide a golf ball using an ionomer resin for an intermediate layer, with an excellent shot feeling, durability and resilience. The present invention provides a golf ball resin composition comprising (A) an ionomer resin consisting of a metal ion-neutralized product of a ternary copolymer composed of an olefin, an α,β-unsaturated carboxylic acid having 3 to 8 carbon atoms and an α,β-unsaturated carboxylic acid ester; (B) a binary copolymer composed of an olefin and an α,β-unsaturated carboxylic acid having 3 to 8 carbon atoms and / or a ternary copolymer composed of an olefin, an α,β-unsaturated carboxylic acid having 3 to 8 carbon atoms and an α,β-unsaturated carboxylic acid ester, and (C) a zinc compound, wherein a content ratio ((A) / (B)) of (A) component to (B) component ranges from 50 / 50 to 80 / 20 in a mass ratio and a content of (C) component ranges from 0.1 part to 20 parts with respect to 100 parts by mass of a sum of (A) component and (B) component, and the golf ball resin composition has a melt flow rate (190° C., 2.16 kg) of 5 g / 10 min or more.

An object of the present invention is to provide a golf ball traveling a great flight distance on driver shots and an excellent shot feeling. The present invention provides a golf ball comprising a spherical core, an intermediate layer covering the spherical core, and a cover covering the intermediate layer, wherein a material hardness (Hm) of a resin composition constituting the intermediate layer ranges from 65 to 80 in Shore D hardness, a material hardness (Hc) of a resin composition constituting the cover ranges from 57 to 72 in Shore D hardness, a hardness difference (Hm−Hc) between the material hardness (Hm) and the material hardness (Hc) is more than 0, and the intermediate layer has a surface hardness satisfying a hardness difference (HmsC−HmsD) between a hardness thereof shown in Shore C hardness (HmsC) and a hardness thereof shown in Shore D hardness (HmsD) of 27 or less.

An object of the present invention is to provide a golf ball resin composition with an excellent resilience and fluidity. Another object of the present invention is to provide a golf ball resin composition with a high hardness and durability. Yet another object of the present invention is to provide a golf ball traveling a great distance with an ionomer cover. The present invention provides a golf ball resin composition comprising, (A) an ionomer resin consisting of a metal ion-neutralized product of a binary copolymer composed of an olefin and an α,β-unsaturated carboxylic acid having 3 to 8 carbon atoms; (B) a binary copolymer composed of an olefin and an α,β-unsaturated carboxylic acid having 3 to 8 carbon atoms, and (C) a zinc compound, wherein a content ratio ((A) / (B)) of (A) component to (B) component ranges from 50 / 50 to 80 / 20 in a mass ratio and a content of (C) component ranges from 0.1 part to 20 parts with respect to 100 parts by mass of a sum of (A) component and (B) component, and the golf ball resin composition has a melt flow rate (190° C., 2.16 kg) of 15 g / 10 min or more.

An object of the present invention is to provide a golf ball intermediate layer resin composition with an excellent resilience and fluidity. Another object of the present invention is to provide a golf ball intermediate layer resin composition with a high hardness and durability. Yet another object of the present invention is to provide a golf ball traveling a great distance with an ionomer intermediate layer. The present invention provides a golf ball intermediate layer resin composition comprising, (A) an ionomer resin consisting of a metal ion-neutralized product of a binary copolymer composed of an olefin and an α,β-unsaturated carboxylic acid having 3 to 8 carbon atoms; (B) a binary copolymer composed of an olefin and an α,β-unsaturated carboxylic acid having 3 to 8 carbon atoms, and (C) a zinc compound, wherein a content ratio ((A) / (B)) of (A) component to (B) component ranges from 50 / 50 to 80 / 20 in a mass ratio and a content of (C) component ranges from 0.1 part to 20 parts with respect to 100 parts by mass of a sum of (A) component and (B) component, and the golf ball intermediate layer resin composition has a melt flow rate (190° C., 2.16 kg) of 15 g / 10 min or more.

An object of the present invention is to provide a golf ball excellent in shot feeling, flight distance and durability. The present invention provides a golf ball comprising a spherical core and at least one cover layer covering the spherical core, wherein the spherical core is formed from a core rubber composition containing (a) a base rubber, (b) a co-crosslinking agent, (c) a crosslinking initiator, and (x) a crosslinked rubber powder; (x) the crosslinked rubber powder contains (x1) soft particles with a hardness difference (Hs−Hp) between a particle hardness (Hp) of the soft particles and a surface hardness (Hs) of the spherical core being 20 or more in JIS-C hardness, and a hardness difference (Hs5−Hp) between the particle hardness (Hp) of the soft particles and a hardness (Hs5) at 5 mm point inside the surface of the spherical core being 15 or more in JIS-C hardness; and the core rubber composition contains (x1) the soft particles in an amount of 1.0 mass % or more.

An object of the present invention is to improve the durability of the golf ball without substantially lowering the spin performance. The present invention provides a golf ball comprising a spherical core and a cover covering the spherical core, wherein the cover contains: (A) a base resin component, and (B) resin fine particles containing a polyrotaxane component having a cyclodextrin, a linear molecule penetrating the cyclic structure of the cyclodextrin in a skewering manner, and blocking groups located at both terminals of the linear molecule to prevent disassociation of the cyclodextrin, wherein at least a part of hydroxyl groups of the cyclodextrin is modified with a caprolactone chain via a —O—C3H6—O— group.

The present invention discloses a soft golf club including a head having a hitting surface to hit a golf ball and a shaft supporting the head, comprising: the head including a through hole horizontally penetrating the hitting surface, a through hole frame defining the through hole, and a mesh portion formed in the through hole in a net form by wires woven with the through hole frame.

An object of the present invention is to provide a novel golf ball material that controls the spin rate on the approach shots while suppressing the change in the spin rate on the driver shots. Another object of the present invention is to provide a golf ball which produces a high spin rate on the approach shots and a low spin rate on the driver shots. The present invention provides a golf ball resin composition comprising: a polyurethane having a polyol component having a number average molecular weight from 200 to 1,500 as a constituting component.

The present invention provides a golf ball comprising a spherical core and at least one cover layer covering the spherical core, wherein the cover is formed from a polyurethane composition containing a polyurethane elastomer as a resin component, the polyurethane composition satisfying properties of rebound resilience of 54% or more and a shear loss modulus G″ of 5.03×106 Pa or less when measured in a shear mode using a dynamic viscoelasticity measuring apparatus at the conditions of the temperature of 0° C., and the oscillation frequency of 10 Hz, and the spherical core has a hardness distribution that R2 of a linear approximate curve determined by a least-squares method is 0.95 or more, when plotting JIS-C hardness measured at a center, a surface and at intervals of 2.5 mm from the center of the spherical core, versus distances from the center of the spherical core.

Golf ball having CoR of at least 0.810, specific gravity SGB of less than 1.00 g / cc, and initial velocity of at least 250 ft / s and comprising a first layer L1, a second layer L2 surrounding L1, and a third layer L3 surrounding L2. L1 is formed from at least one highly neutralized polymer and has first specific gravity SG1; L2 is formed from at least one partially neutralized polymer and has second specific gravity SG2; and L3 is formed from at least one of a thermoset or thermoplastic composition and has third specific gravity SG3. At least two of SG1, SG2, and SG3 is less than 1.13 g / cc. SG1 may be less than 1.13 g / cc, or less than 1.0 g / cc. The thermoset or thermoplastic composition may comprise polyurethane(s), polyurea(s), polyurethane(s) / polyurea(s) hybrids, and / or ionomers such as at least partially neutralized polymers and / or HNPs.

An object of the present invention is to provide a golf ball excellent in shot feeling, flight distance and durability. The present invention provides a golf ball comprising a spherical core and at least one cover layer covering the spherical core, wherein the spherical core is formed from a core rubber composition containing (a) a base rubber, (b) a co-crosslinking agent, (c) a crosslinking initiator, and (x) a crosslinked rubber powder; (x) the crosslinked rubber powder contains (x1) soft particles with a hardness difference (Hs−Hp)between a particle hardness (Hp) of the soft particles and a surface hardness (Hs) of the spherical core being 20 or more in JIS-C hardness, and a hardness difference (Hs5−Hp) between the particle hardness (Hp) of the soft particles and a hardness (Hs5) at 5 mm point inside the surface of the spherical core being 15 or more in JIS-C hardness; and the core rubber composition contains (x1) the soft particles in an amount of 1.0 mass % or more.

A fuel cell power pack for a drone according to the present invention comprises: a power pack body to be coupled to a drone; a fuel cell stack module installed within the power pack body so as to supply electricity to the drone by being fed with fuel and air; a state information detection unit for detecting state information of the fuel cell stack module; a power pack communication unit for transmitting information outside the power pack body or receiving information from a source outside the power pack body by cable or wirelessly; and a power pack controller for controlling the power pack communication unit to transmit the state information of the fuel cell stack module, detected by the state information detection unit, outside the power pack body.

A UAV flight control system, including a main controller, an actuator, communication equipment, ground station equipment, the main controller includes a data acquisition module, a data processing module, a communication module, the data acquisition module collects the measurement signals of each sensor, and Upload to the data processing module; the data processing module manages and controls various flight modes and actuators in the UAV; the actuator includes the motor, electric adjustment device and spraying device; the ground station equipment tracks the multi-UAV Planning, formation and collaborative planning of heterogeneous multi-UAVs, the main controller realizes the control of UAVs' ground imitation flight control, highly reliable fault-tolerant control and autonomous obstacle avoidance.