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113 results about "Satellite downlink" patented technology

System using leo satellites for centimeter-level navigation

Disclosed herein is a system for rapidly resolving position with centimeter-level accuracy for a mobile or stationary receiver [4]. This is achieved by estimating a set of parameters that are related to the integer cycle ambiguities which arise in tracking the carrier phase of satellite downlinks [5,6]. In the preferred embodiment, the technique involves a navigation receiver [4] simultaneously tracking transmissions [6] from Low Earth Orbit Satellites (LEOS) [2] together with transmissions [5] from GPS navigation satellites [1]. The rapid change in the line-of-sight vectors from the receiver [4] to the LEO signal sources [2], due to the orbital motion of the LEOS, enables the resolution with integrity of the integer cycle ambiguities of the GPS signals [5] as well as parameters related to the integer cycle ambiguity on the LEOS signals [6]. These parameters, once identified, enable real-time centimeter-level positioning of the receiver [4]. In order to achieve high-precision position estimates without the use of specialized electronics such as atomic clocks, the technique accounts for instabilities in the crystal oscillators driving the satellite transmitters, as well as those in the reference [3] and user [4] receivers. In addition, the algorithm accommodates as well as to LEOS that receive signals from ground-based transmitters, then re-transmit frequency-converted signals to the ground.
Owner:INTEGRINAUTICS

Integration high speed remote sensing data receiving and processing equipment

The invention relates to integrated high-speed remote sensing data receiving and processing equipment. When the equipment is used to receive data, satellite downlink serial data are converted into parallel data through serial-parallel conversion and are sent into a frame synchronous processing module for frame synchronous treatment, frame synchronization characters are searched, fault-tolerant parameters are calculated, frame synchronization signals are generated according to the frame length and the frame synchronization characters, and the frame synchronization signals and data frame are sent to a combined decode module. The combined decode module performs descramble, RS decoding and CRC check processing on the data frame according to the frame synchronization signals, and sends the data to a cache. The data in the cache are subjected to data synthesis and wave filtering processing to be sent into a data distribution module. The data distribution module sends the transmitted data into a load imaging and processing module for format analysis processing, performs classified processing on the data according to load category, and displays the data in real time. When the data are sent, uplink data are sent into the cache through a data distribution module, a combined coding module reads the data from the cache, performs scrambling, RS coding and CRC check processing on the data, sends the data into a parallel-serial conversion module, converts the data into the serial data and transmits the data to a satellite.
Owner:SPACE STAR TECH CO LTD

Dual-mode positioning time-service type receiver for compass satellite and global positioning system (GPS) satellite

The invention discloses a dual-mode positioning time-service type receiver for a compass satellite and a global positioning system (GPS) satellite. The receiver comprises an antenna module, a radio frequency channel module, a compass processing module, a GPS processing module and an expansion board module, wherein the antenna module comprises a compass receiving antenna, a compass transmitting antenna and a GPS receiving antenna; the compass receiving antenna is used for receiving a compass satellite downlink signal; a compass downlink radio frequency navigation signal is acquired by filtration of a filter and amplification of a compass low-noise amplifier; the compass transmitting antenna receives the signal which is transmitted by a compass power amplifier and transmits a signal to the compass satellite in the sky; and the GPS receiving antenna is used for receiving a GPS satellite downlink signal. The invention provides the receiver which receives the signals of the compass satellite and the GPS satellite simultaneously, so that functions of compass time service, compass positioning, GPS time service and GPS positioning can be realized, the receiver is independent of the GPS, and the safety and stability of civil basic industries of our country are improved.
Owner:SHAANXI NAVI INFORMATION TECH

Modulation performance test method for navigational satellite binary offset carrier signal

ActiveCN102638319AAvoid influenceSolve the problem that the baseband modulation characteristics cannot be tested by the vector signal analysis methodTransmission monitoringFrequency spectrumCarrier signal
The invention discloses a modulation performance test method for a navigational satellite binary offset carrier signal. The modulation performance test method comprises the following steps of: firstly, carrying out direct A/D sampling on a BOC (binary offset carrier) modulation navigation signal of a navigational satellite downlink transmission microwave frequency band; then, carrying out variable-frequency filtering and hilbert transform on the signal in a numeric field; carrying out quadrature demodulation, channel gain compensation and phase compensation processing in digital communication, and filtering by a measurement filter to obtain measured data; carrying out symbol detection, reference signal generation processing and reference filtering on the measured data to obtain reference data; and calculating the reference data and the measured data to obtain a parameter and a signal graph which reflects the base band modulation performance. The BOC carrier modulation signal is processed in the numeric field by the modulation performance test method. Because a BOC single sideband frequency spectrum is extracted in the numeric field, the problem that the BOC signal can not be subjected to the modulation characteristic test through a vector signal analysis method because of subcarrier can be solved.
Owner:BEIJING INST OF SPACECRAFT SYST ENG

An earth observation satellite mission effectiveness evaluation index system and an analysis method

The invention relates to an earth observation satellite mission effectiveness evaluation index system and an analysis method. The system comprises a mission completion degree index, a time response degree index and a resource utilization rate index. The task fulfillment index comprises a regional target coverage rate, a total task fulfillment rate, a moving target recognition degree, a moving target tracking track fit degree, a task fulfillment benefit and a credibility of a moving target search result. The aging responsiveness index comprises a task response time and a time resolution. The resource utilization index comprises a satellite payload rate, a total satellite side swing number, a total startup time, a total startup number, a large-capacity memory occupancy rate, a ground stationand a relay satellite downlink window utilization rate. The method of the invention can fully embody the physical connection between the operation logic of the system and the indexes, and the evaluation result is intuitionistic, readable and understandable, the method of the invention is an evaluation method with practical physical significance and effectively overcomes the subjectivity and fuzziness existing universally in the efficiency evaluation process.
Owner:TECH & ENG CENT FOR SPACE UTILIZATION CHINESE ACAD OF SCI

Method for combining tri-band code wave pseudorange with carrier phase in satellite navigation and positioning

The invention provides a method for combining a tri-band code wave pseudorange with a carrier phase in satellite navigation and positioning, relating to the technology of the satellite navigation and positioning. The method comprises the following steps of: using terminal equipment to receive the satellite downlink three code wave pseudoranges and the carrier phase; obtaining a code wave combined pseudorange and a carrier combined phase according to an integral coefficient combination, selecting a positive combination coefficient or a negative combination coefficient according to the principle that the time which is influenced by an ionosphere for closing to and solving ambiguity is short, and fast solving the ambiguity by the positive combination or the negative combination; and according to the principle that an ionosphere influence in a satellite-ground distance can be fast removed, selecting the combination coefficient to set up a double positive combination carrier wave which is used for removing the ionosphere influence in the satellite-ground distance, and using more than four (including four) pseudorange observation equations to solve the real position of the receiving terminal. The invention can set up a new system which not only can realize the high dynamic state of the code wave but also has the high precision of the carrier wave.
Owner:NAT ASTRONOMICAL OBSERVATORIES CHINESE ACAD OF SCI +1

Power distribution method and power distribution device for downlink of low-earth-orbit satellite

ActiveCN111867104ASolve the problem of low capacityAccelerating the Convergence Speed ​​of Reinforcement LearningTransmission path divisionCriteria allocationFrequency spectrumSpectral efficiency
The invention provides a power distribution method for the downlink of a low-orbit satellite. The method comprises the steps of: initializing the low-orbit satellite, and building a Markov decision process; observing the current state St; randomly selecting an action or selecting an optimal action according to the probability of an exploration factor; obtaining a new state St+1 and the instant reward rt of the current state St according to an action at, and storing the (st, at, rt, st+1) tetrad into an experience pool; under the condition that a cycle period is greater than a training number,training a current network; under the condition that the current time slot is integer multiples of the updating frequency of a target network, updating parameters of the target network; adding 1 to the current time slot; repeating the above steps until the current time slot is greater than a time slot counter, setting the current time slot to be 1 and adding 1 to the count of the cycle period; andrepeating the steps until the cycle period is greater than the training network period number. According to the distribution method, a deep reinforcement learning algorithm is adopted to dynamicallydistribute the subcarrier power of the multi-beam low-orbit satellite, so that the capacity of the low-orbit satellite is maximized, and the spectral efficiency is improved.
Owner:SHANGHAI INST OF MICROSYSTEM & INFORMATION TECH CHINESE ACAD OF SCI

A satellite telemetry parameter allocation and scheduling method

ActiveCN106688332BSatisfy the application of on-orbit telemetry strainImprove test efficiencyElectric signal transmission systemsRadio transmissionCollection periodEngineering
The invention provides a satellite telemetry parameter allocation and scheduling method, including: step 1, the upper computer collects the whole satellite telemetry parameters from the lower computer, and the collection period is equal to the operation cycle of the upper computer; step 2, designs the telemetry frame format, and divides into fixed telemetry areas In the subcontracting telemetry area, the upper computer performs grouping according to the format of the telemetry frame; step 3, design a large table of telemetry data frames, and the upper computer performs grouping and downloading of telemetry data according to the large table of telemetry data frames. The present invention realizes the dynamic scheduling capability of satellite downlink telemetry data through the method of centralized allocation of telemetry parameters of the satellite upper computer, and can conveniently increase the downlink rate of the telemetry parameters of the tested system through the way of uplink injection during the satellite test process, It can more effectively judge the state of the test system, and can focus on downloading different telemetry parameters according to the different stages of the satellite in orbit, and realize the ability to download key telemetry parameters in different working modes.
Owner:SHANGHAI SATELLITE ENG INST

Rapid satellite locking method of portable satellite receiver

InactiveCN104125002AEasy to useCoarse adjustment is fastRadio transmissionSatelliteSignal intensity
The invention discloses a rapid satellite locking method of a portable satellite receiver. Coarse tuning contains the following steps: position of the receiver is determined; a satellite which is expected to be locked is selected; pitch angle, azimuth angle and polarization angle of the satellite relative to the receiver are calculated; and angle of the receiver is adjusted manually. Fine tuning contains the following steps: a downlink beacon signal of the satellite is received and satellite signal power within adjustable bandwidth is calculated; signal maximum power point is obtained; pitch angle and azimuth angle of the receiver are finely-tuned so as to be directed at the maximum power point; and polarization angle is finely-tuned and the maximum power point is observed, and the polarization angle which maximizes power is selected. An interface of a visualized terminal displays signal intensity within bandwidth during the fine-tuning process at real time and visually shows whether the result of the fine-tuning operation is accurate. The fine-tuning operation is convenient and fast. The downlink beacon signal of the satellite is received so as to realize measurement of the signal intensity. It is not necessary to transmit signals by antennas. The influence of adjacent satellite interference can be avoided effectively. Accuracy of satellite signal intensity measurement is higher.
Owner:成都国恒空间技术工程股份有限公司

Communication satellite frequency spectrum monitoring equipment and frequency spectrum acquisition and feature identification method thereof

The invention discloses communication satellite frequency spectrum monitoring equipment and a frequency spectrum acquisition and feature identification method thereof, and belongs to the technical field of satellite communication and frequency spectrum monitoring. The equipment realizes long-term monitoring of GEO communication satellite signals, acquires and automatically stores each satellite signal spectrogram in real time, completes statistical analysis of resource utilization and carrier distribution related to each satellite signal, and provides a basis for resource scheduling and network optimization of a satellite communication system; effective identification of satellite carrier signal parameters is realized, legality inspection of carrier signals is completed, an alarm is givenin time when abnormity is found, and support is provided for autonomous operation and troubleshooting of the system; and interference monitoring of satellite signals is realized, accurate identification and automatic alarm of interference parameters are completed, and a reference is provided for anti-interference decision making of the system. Two paths of satellite downlink signals within the frequency range of 70-6000MHz can be received at the same time, and the functions of frequency spectrum generation, parameter identification, interference monitoring and the like are completed on the received signals.
Owner:南京御通信息技术有限公司
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