64 results about "Pilot training" patented technology

The present invention relates to a digital video recording system for use on an aircraft. The digital video recording system is configured with the same form factor as an analog video recording system to enable a direct hardware replacement. In addition the digital video recording system in accordance with the present invention is configured to emulate all of the functions of an analog video recording system including the ability to overwrite the existing data. By emulating the functions of an analog video recording system, aircraft which include cockpit controls for an analog video recording system can be reused with the newer digital video recording system. As such replacement of analog video recording systems is virtually seamless and does not require pilot training.

The invention belongs to the field of aviation training, relating to a flight training data acquisition and quality evaluation system of an analog machine and a technical scheme thereof, in particular to the problems of acquiring the videos of flight data in a training system monitor of the analog machine, preprocessing an image after video frame graduation by applying an image processing technology, recognizing the flight data in the image by using a pattern recognition technology, carrying out three-dimensional simulation on a flight path in the training process of the analog machine so as to further carry out teaching evaluation, generalizing and summarizing typical problems, submitting the problems and flight training videos to a video server and providing a share and study platform. Under the conditions of keeping fully isolation with an analog machine system and avoiding a data communication channel with the analog machine system, the flight training data acquisition and quality evaluation system provided by the invention accurately acquires the flight data, reproduces the training process of a pilot and evaluates the quality.

A Flight Risk Management System (“FRMS”). The system provides supplementary preflight and in-flight guidance to relatively inexperienced owner/operators of high performance aircraft. A pilot wishing to enroll in the FRMS must have an aircraft equipped with an in-flight data recorder capable of monitoring the aircraft's state and communicating this state to an FRMS dispatcher. The dispatcher analyzes each flight before its commencement and imposes restrictions designed to promote flight safety. The dispatcher monitors the flight in progress to ensure the pilot's compliance with all directives. For most enrollees, participation in the FRMS is a mandatory condition precedent to the pilot's insurance coverage. Thus, the potential loss of insurance coverage enforces compliance. In the preferred embodiment, the FRMS manages pilot training, pilot performance, aircraft maintenance, and flight risk assessment.

In accordance with aspects of the present invention, a method, apparatus and system for learning antenna weighting factors in a communication system including relay nodes. In one embodiment, an apparatus (e.g., a relay node (325)) for use with a communication system includes a first antenna (330) configured to receive a first signal including a pilot training sequence from a source node (305) and a second signal including a power-based feedback signal or a signal-to-noise based feedback signal from a destination node (350). The apparatus also includes a second antenna (335) configured to transmit at least a portion of the first signal with an antenna weighting factor (e.g., a perturbed antenna weighting factor). The apparatus further includes an antenna weighting factor module (340) coupled to the first antenna (330) and configured to iteratively adjust the antenna weighting factor in response to the second signal.

The present invention relates to software for training an aircraft pilot to respond to the failure of one or more engines of a multi-engine aircraft during flight. The software simulates engine failure through the use of software imposed power output limits on the one or more engines for which failure is simulated. In certain embodiments, the software of the present invention sets one or more of the engine condition gauges to a fictitious readings corresponding to readings that would be displayed in the event of an actual engine failure.

The invention discloses a three dimensional virtual simulation system and simulation method for shipboard aircraft pilot training injury assessment. The three dimensional virtual simulation system comprises a hardware platform, a bottom layer support model base, a data management module, a bio-mechanical simulation module, a three dimensional virtual scene view module and a post processing module. The three dimensional virtual simulation method comprises: the data management module receives the data and configuration parameters input by a user, and transmits configuration parameter management to the bio-mechanical simulation module and the three dimensional virtual scene view module; the obtained bio-mechanical simulation data is transmitted to the post processing module and the three dimensional virtual scene view module respectively; three dimensional virtual scene view simulation is carried out and the result is stored; and by means of comprehensive comparison between the three dimensional virtual scene view simulation data and the bio-mechanical simulation data, the training injury assessment result for pilots are displayed and analyzed to the user. The three dimensional virtual simulation system and simulation method for shipboard aircraft pilot training injury assessment solve the defects of nonrepeatability and high risk of a traditional experimental study, and have the advantages of being high in efficiency, having repeatability and being low in cost.

The invention relates to a pilot training control method based on pilot comprehensive capability evaluation, and belongs to the field of flight safety. The method comprises the following steps: firstly, determining a pilot comprehensive capability evaluation index, constructing an evaluation index hierarchical structure model, and forming an evaluation index system consisting of a target layer, acriterion layer and an index layer; then, according to the relative importance degree of the evaluation indexes, pairwise comparing and judging the evaluation indexes of the same layer, and establishing a relative importance judgment matrix; carrying out consistency inspection on the judgment matrix; calculating the weight of each evaluation index; and finally, carrying out standardized processingon the measurement parameters of each evaluation index, evaluating the comprehensive capability of the pilot by adopting a weighted statistical method, and finally obtaining a weak link of the pilotaccording to an evaluation result and establishing a training scheme. Compared with the prior art, the method can comprehensively and systematically represent various factors influencing pilot comprehensive capability evaluation and the mutual relation among the factors, and is wide in application range and accurate in evaluation.

The invention discloses a frequency domain arrival detection method of an orthogonal frequency division multiplexing system. A frequency domain synchronous transmitting unit adopts two frequency domain pseudorandom sequences with identical length but different phases, a zero is respectively compensated to each pseudorandom sequence to obtain a pseudorandom expanded sequence, then rapid Fourier inverse transformation operation is carried out on the pseudorandom expanded sequences to obtain time domain sequences, and then the two time domain sequences are cascaded to obtain a synchronous pilot training sequence. A frequency domain synchronous receiving unit adopts a time window with a length being identical to that of one pseudorandom expanded sequence, rapid Fourier transformation operation is carried out on data inside the window, then the data is correlated with a known local pseudorandom expanded sequence after being subjected to peak clipping and amplitude limitation processing, and the signal arrival is judged by utilizing excellent autocorrelation property of the pseudorandom sequence and simultaneously considering a threshold and position-based detection method. Due to the adoption of the frequency domain arrival detection method of the orthogonal frequency division multiplexing system, interference of a single tone, narrow band and the like can be effectively resisted, and reliable signal arrival detection can also be realized under a severe channel condition.

The invention relates to a multi-cell channel estimation method and a device. The embodiment of the multi-cell channel estimation method comprises the steps of obtaining a pilot training sequence of all users of a local cell and neighbor cells, and using the obtained pilot training sequence to construct a matrix; utilizing the pilot training matrix for calculating channel estimation results; and separating the channel estimation results of all users of all cells which correspond to a receiving antenna from the channel estimation results. The utilization of the invention can accurately calculate the channel estimation of the local call, calculate the channel estimation results of the neighbor cells, further effectively improve the channel estimation performance and improve the capacity andthe throughput of a system.

The invention relates to a method for searching an optimal pilot length and a power division factor in a point-to-point MISO SWIPT system, comprising the following steps of: (1) performing uplink channel estimation by a first time slot TauT, namely sending a pilot training sequence by a receiving end, and performing channel estimation based on the minimum mean square error MMSE by a sending end; (2) performing downlink information and energy transmission by a second time slot (1-Tau)T; (3) analyzing channel estimation errors; (4) modeling and analyzing problems; and (5) searching the optimal pilot length and power division factor. The invention analyzes the joint optimization between the length of the pilot sequence performing the channel estimation and the power division factor of the receiving end, thereby obtaining the optimal pilot length enabling the system to reach the maximum rate, and corresponding power division factor.

The present invention provides a system for training a subject to recognise the onset of hypoxia, the system including (i) a flight simulation system, and (ii) a hypoxia induction system, wherein the flight simulation system is operably linked to the hypoxia induction system. The system provides a tool for pilot training to a pilot, allowing for the delivery of standardised training programs where the tasks required for the operation of an aircraft are able to be coordinated with an induction of hypoxia in the subject. Such a system is also able to provide an assessment tool to demonstrate when a pilot has had sufficient training in recognising the effects of hypoxia.

The invention discloses a flight teaching management system, including a teaching management subsystem and an integrate playback and scoring subsystem. The teaching management subsystem comprises a curriculum design module which enables a teacher to conduct four-dimensional curriculum design, a teacher control module which enables the teacher to randomly select one or more students to set a temporary flight situation in the flight training process, a student management module which manages student information, curriculum information and teaching and training planes, and an asset management module which uniformly manages all equipment in a teaching platform. The integrate playback and scoring subsystem comprises a playback module and a scoring module. The playback module loads assigned data in a data record server database, and selects an assigned student for data playback after loading the data. The scoring module accesses to data of an assigned data form in a record database of a data record server and prints and displays the data in a graphical manner. The integrate playback and scoring subsystem achieves playback and scoring of pilot training correlated videos.

The invention discloses a Robinson R44 helicopter multi-task flight training device which is mainly used for practical flight simulation training. Taking the standard requirements of a CCAR-60 helicopter flight training device four-grade certificate, and selecting a Robinson R44 helicopter as a template, a helicopter flight training device is developed. A helicopter cockpit and a helicopter instrument system provide 1:1 Robinson R44 type helicopter cockpit simulation and flight state presentation. The training device mainly comprises the helicopter cockpit, the helicopter instrument system, aninterface system, a control rod force load system, a flight dynamics simulation system, a helicopter system simulation system, a visual scene system, an operator console, a sound effect system, QTG test software or other 10 main sub-systems. The device is high in simulation degree, has the function of pilot training, and can be popularized in the civil aviation industry.

Embodiments of the present invention provide a method and a device for detecting a pilot attack, electronic equipment and a storage medium. The method for detecting the pilot attack is applied to a legal user side and comprises the following steps of sending a first pilot signal to a transmitting end in an uplink stage of pilot training in order to make the transmitting end obtain each first peakvalue corresponding to a spatial spectrum function of each first pilot signal sent by each user side; receiving each first peak value sent by the transmitting end in a downlink stage of pilot trainingand each second pilot signal transmitted by the transmitting end and other user sides in order to obtain a spatial spectrum function of each second pilot signal about a scanning angle of the legal user side; obtaining each second peak value corresponding to the spatial spectrum function; and determining the first peak value corresponding to a minimum difference as a spatial spectrum of the legaluser side, determining the second peak value corresponding to the minimum difference as a spatial spectrum of the transmitting end, and determining the remaining peak values as the spatial spectrums of the malicious user sides respectively. According to the embodiments of the invention, a purpose of identifying the malicious user side is achieved.

The invention discloses an approach stability assessment method based on energy management. The method comprises the following steps that: S1: collecting flight data, and extracting parameters used for approach stability assessment; S2: utilizing two parameters including flight height and ground velocity to calculate energy height; S3: calculating an energy conversion boundary condition function in an approach to landing process of the airplane; and S4: through a difference value of the energy height and the energy conversion boundary condition function in the approach to landing process of the airplane, judging approach stability. By use of the method, an energy management concept is used for designing a stable approach assessment standard and a relationship between an unstable approach and energy, a basis is provided for unsafe incident monitoring and risk identification, the identification accuracy of the unstable approach can be effectively improved, a reference is provided for flight risk identification and pilot training, and safety management levels and training efficiency can be effectively improved.

The invention discloses a semi-physical water throwing and drawing fire extinguishing simulation evaluation system for an amphibious fire extinguishing aircraft. The system comprises a flight simulator, a fire extinguishing task scene construction module and fire extinguishing flight simulation software. The flight simulator is connected with the fire extinguishing flight simulation software and the fire extinguishing task scene construction module through a network, and the fire extinguishing task scene construction module is directly connected with the flight simulator. And the flight simulator transmits the operation quantity into fire extinguishing flight simulation software, and the fire extinguishing flight simulation software obtains flight data through calculation. And the fire extinguishing task scene construction module calculates the flight data, generates picture information, and collects fire extinguishing effect related data for fire extinguishing effect evaluation by fire extinguishing flight simulation software. The flight simulator capable of simulating fire extinguishing flight simulation can accurately simulate the whole flight process of an amphibious fire extinguishing aircraft and show the fire extinguishing process. A fire extinguishing simulation evaluation system is constructed, the fire extinguishing effect of the pilot can be evaluated, and the systemhas wide application prospects in the aspects of pilot training and the like.

The invention relates to a closed three-dimensional vestibule training device which comprises a support, an outer side ring, a middle ring and an inner side ring. In the initial state, three rotatingrings are in the state of sharing the same circle center and the same plane. The support and the outer side ring are connected through a rotating pair, the outer side ring and the middle ring are connected through a rotating pair, and the middle ring and the inner side ring are connected through a rotating pair, and the angle formed between the rotating axis of the inner side ring inside the middle ring and the rotating axis of the middle ring inside the outer side ring is 90 degrees. The angle formed between the rotating axis of the middle ring inside the outer side ring and the rotating axisof the outer side ring inside the support is 45 degrees. The diameters of the outer side ring, the middle ring and the inner side ring are sequentially reduced, and a safety device is arranged on theinner side ring. Due to multi-dimensional rotation, the high speed, complex steering, G increase and decrease and other flight transportation actual environment can be simulated, and training betterfits the actual working requirement, and better fits vestibule resistance and adaptability needed by the complex environment. The closed vestibule training device is wide in application range, can beapplied to the civil aviation flight major and flight attendant, air marshal and air duty majors directly related to flight transportation, and can be applied to military aviation pilot training, navigation shipping and other major training. The device can be applied to physical education, physical exercise, physical ability training practice, physical ability testing and experiments and other working in various majors.

A flight training quality and efficiency evaluation method fusing physiological data and flight parameter data comprises the following steps: firstly, collecting physiological data and psychological state data in a flight process of a pilot, and then constructing a psychological state prediction model by using the collected physiological data and psychological state data based on an SVM (Support Vector Machine) method; the psychological state of the pilot in the flight process is analyzed through the psychological state prediction model, and meanwhile, the flight parameter data in the flight process is combined to quantify the analysis result, so that comprehensive evaluation of the flight training quality and efficiency of the pilot is achieved. The psychological state prediction model is constructed based on the SVM method so as to analyze the physiological data of the pilot, the psychological state of the pilot is comprehensively and accurately analyzed, meanwhile, flight training is evaluated from multiple angles in combination with a flight parameter quantitative analysis result, scientific method support is provided for pilot training quality and efficiency evaluation, and the pilot training quality and efficiency evaluation efficiency is improved. The method provides support for rapid training and efficient flight training of pilots, and provides a basis for aviation colleges to optimize a scientific training scheme.

The present disclosure provides for a system for rapidly generating minimum length pilot training schedules which uses a branch and bound, and a mixed integer programming model with constraints to produce student and resource schedules at a device period level for all pilots of an airline.

The invention relates to a massive MIMO system configuration and verification method based on multiple sub-antenna arrays. The configuration method includes the following steps: configuring a corresponding number of sub-antenna arrays according to the number of sectors uniformly divided by a service area of a massive MIMO system, wherein each sub-antenna array serves one sector correspondingly; configuring the number of antennae of each sub-antenna array according to the density of clients in each sector; obtaining an observation matrix based on mutually orthogonal pilot training sequence information that is sent by all the clients in the service area and is received by a base station end, and the total number of the antennae of the base station end, and estimating channel state information in combination with the observation matrix; and enabling the base station end to perform downlink wireless communication transmission by using the estimated channel state information and a maximum ratio transmission precoding method. According to the scheme of the invention, the energy consumption and the complexity of hardware implementation can be effectively reduced, and the spectrum efficiency of the system can also be ensured.

A device for pilot training includes a memory, an interface, and one or more processors. The memory is configured to store at least one computational model of at least one human sensory system. The interface is configured to receive sensor data and aircraft state data from a flight simulator. The sensor data includes pilot activity data and motion data. The motion data is indicative of detected motion of a simulated aircraft of the flight simulator. The processor(s) are configured to process the motion data and the pilot activity data based on the at least one computational model to predict a pilot estimated aircraft state. The processor(s) are configured to determine an estimated error based on a comparison of the pilot estimated aircraft state and a detected aircraft state. The aircraft state data indicates the detected aircraft state. The processor(s) are configured to provide the estimated error to a second device.

The invention provides an airplane system capable of realizing flight experience. The airplane system comprises an airplane which comprises a flight deck, an airplane body and flying wings. A blower is arranged in front of the airplane body. The blower is provided with blades. A fixing rod is arranged between the blower and the airplane body. A position-limiting rope is arranged between the front end of the airplane body and the fixing rod. A height-limiting rope is arranged between the airplane body and the ground. The blades of the blower rotate to drive the flying wings to work so that the airplane body is enabled to upwardly suspend. Early-stage pilot training and providing of the flight experience can be realized, and the airplane system has characteristics of low cost and high safety coefficient. The blades of the blower rotate to drive the flying wings to work so that the airplane body is enabled to upwardly suspend. The airplane system can be used for early-stage pilot training and providing a real flight experience in life of people. The airplane system is low in manufacturing cost, high in safety performance and relatively high in popularization value.

The invention provides a crosstalk estimation method, device and system. In the crosstalk processing method, device, and system provided by the embodiments of the present invention, the transceivers of the lines respectively generate pilots in different spectrum ranges that meet the preset relationship with the pilot training signals of other lines according to the pilot sequences allocated by the vectoring control entity. Frequency training signal, so that the receiver of the line can determine the sample error according to different pilot training signals, so that the vectorization control entity can determine the crosstalk channel coefficient of the in-band spectrum and out-of-band spectrum of other lines to the line, so that by Precoding the data signal to be sent on this line can eliminate the influence of other lines on the crosstalk between the in-band and out-of-band spectrum of the line, and reduce the impact of crosstalk between lines on the line rate in a system where lines with different attributes coexist. Influence, thereby increasing the effect and stability of FTTC speed-up.