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68 results about "Link margin" patented technology

In a wireless communication system, the link margin (LKM), measured in dB, is the difference between the receiver's sensitivity (i.e., the received power at which the receiver will stop working) and the expected minimum received power. A 15 dB link margin means that the system could tolerate an additional 15 dB of attenuation between the transmitter and the receiver, and it would still just barely work.

Near-earth remote sensing satellite self-adaptive variable code modulation data transmission system and method

The invention discloses a near-earth remote sensing satellite self-adaptive variable code modulation data transmission system and method, belonging to the field of satellite overall design. The invention provides a variable code modulation data transmission system and method based on a DVB-S2 protocol, which fully utilizes link resources for the near-earth remote sensing satellite data transmission, adopts a variable code modulation (VCM) system, fully utilizes the system link margin, and improves the satellite star-ground data transmission efficiency; and the optimal code modulation mode is selected by means of the DVB-S2 protocol under the condition of satisfying a bit error rate and the link margin, so that the amount of effective information transmitted per unit time is the largest. The near-earth remote sensing satellite self-adaptive variable code modulation data transmission method provided by the invention can maximize the adaptation to changing channel conditions and channel capacity due to orbital changes of the near-earth remote sensing satellite, and transmit more data information on a limited spectrum resource, which is very suitable for the data transmission of the near-earth remote sensing satellite to the ground.
Owner:BEIJING INST OF SPACECRAFT SYST ENG

Self-adaptive distance data transmission method for aircraft-mounted terminal

The invention provides a self-adaptive distance data transmission method for an aircraft-mounted terminal and aims to provide a data transmission method capable of improving transmission link utilization rate and data transmission efficiency and also provides a self-adaptive implementation method for the data transmission between the aircraft-mounted terminal and a data transmission receiver. The self-adaptive distance data transmission method is realized through the following technical scheme: an aircraft inertial navigation system provides inertial navigation data for the aircraft-mounted terminal in real time through a serial port, a link margin estimator of the aircraft-mounted terminal calculates the distance between an aircraft and the data transmission receiver in real time according to the inertial navigation data and works out the system margin of the data transmission link according to the stored data transmission receiver relevant parameters, the data transmission link parameters and the parameters such as the EIRP (effective isotropic radiated power) value of the antenna of the aircraft-mounted terminal, the aircraft-mounted terminal automatically selects data transmission speed, carries out coded modulation on data in different data transmission speeds through an encoder and a modulator, and transmits the data to the data transmission receiver after up-conversion and amplification processing.
Owner:10TH RES INST OF CETC

Method for analyzing working performance of damaged satellite-earth data transmission antenna

ActiveCN104467987AComprehensive assessment of work performance impactEase of evaluationTransmitters monitoringTerrainAntenna polarization
A method for analyzing the working performance of a damaged satellite-earth data transmission antenna comprises the steps of (1) calculating the equivalent isotropic radiated power (EIRP) of a satellite according to the output power of a satellite transmitter, satellite antenna gain and the transmission channel loss value; (2) calculating the maximum slant range R of signal transmission according to the mean terrain level of a satellite and the minimum elevation of a ground receiving antenna; (3) calculating the free space loss Lf of a signal according to the downlink carrier frequency of the satellite data transmission signal and R; (4) calculating all transmission losses L of the data transmission signal according to the atmosphere loss, the directivity loss of the receiving antenna, the polarization loss and atmosphere value of the receiving antenna and Lf; (5) calculating the bit signal to noise ratio of a received signal by means of the coding gain, the transmission code rate, the coding rate and the link margin; (6) calculating the bit signal to noise ratio actually needed by the received signal according to bit error rate requirements so as to obtain the channel margin, wherein if the margin is positive, the overall performance of the damaged data transmission antenna can still meet the requirements of a system, and the working performance of the data transmission antenna is affected otherwise.
Owner:CHINA ACADEMY OF SPACE TECHNOLOGY
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