GATED RANGE SCANNING LFMCW RADAR STRUCTURE
    1.
    发明申请

    公开(公告)号:US20180329047A1

    公开(公告)日:2018-11-15

    申请号:US15344365

    申请日:2016-11-04

    CPC classification number: G01S13/34 G01S7/354 G01S13/18 G01S13/343

    Abstract: The present disclosure provides a gated range scanning linear frequency modulated continuous wave (LFMCW) radar structure, including: a frequency synthesizer, a first mixer, a second mixer, a first filter, and a third mixer. The frequency synthesizer is configured for generating a first local oscillating signal and a second local oscillating signal, a frequency of the first local oscillating signal varying in a frequency range, each frequency corresponding to a sub-range of a coverage range scanned by the LFMCW radar structure. The first mixer is configured for mixing a copy of a transmitted signal and the first local oscillating signal to generate a first output signal (the receiver's first local oscillator). The second mixer is configured for mixing the first output signal and a received signal from a receiving antenna to generate a second output signal that includes an intermediate frequency (IF) signal being received by the first filter.

    SYSTEM AND METHOD FOR SPACE SITUATIONAL AWARENESS DEMONSTRATION

    公开(公告)号:US20180268605A1

    公开(公告)日:2018-09-20

    申请号:US15971940

    申请日:2018-05-04

    CPC classification number: G06T1/20 B64G7/00 G06T2210/52 G08G99/00

    Abstract: Methods and systems for space situational awareness (SSA) demonstration are provided. The system includes a space data collector component, for collecting space initialization data of space objects from initialized space sources and pre-processing the space initialization data; a data relocation component, for distributing the space initialization data pushed from the space data collector component into multiple streaming channels for streaming; a streaming platform, for streaming, mapping, and reducing the space initialization data from the data relocation component to provide streamed data; a real-time analysis component, for calculating the streamed data to conduct a real-time detecting and tracking analysis of the space objects by implementing algorithms for one or more of space uncertainty propagation, space object tracking, sensor management, and collision avoidance; and a space visualization component, for displaying a visualization of space situational awareness (SSA) based on analyzed results from the real-time analysis component.

    SATELLITE COMMUNICATION FRAMEWORK AND CONTROL METHOD THEREOF

    公开(公告)号:US20200266883A1

    公开(公告)日:2020-08-20

    申请号:US16275859

    申请日:2019-02-14

    Abstract: A satellite communication framework includes a satellite system controller; at least one satellite transponder; and a plurality of remote terminals, each including a modem, a router, and a terminal agent. The terminal agent is configured to, based on a current allowable data rate and measurements of a current router queue size and a current router packet arrival rate, use a delayed uplink resource assignment for each modem and an MCV-based flow-control policy to forecast a future router queue size and a future router packet arrival rate and further update the delayed uplink resource request for a time after an uplink allocation delay. The modem is configured to communicate with the router and also with the satellite system controller through the satellite transponder, perform modulation and demodulation, and manage packet loss and delay according to the future router queue size and the future router packet arrival rate.

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