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    blocking oscillator

    Abstract: superheterodyne transceiver UMTS beamforming transceiver rf wcdma rake receiver sample IS-95 mux space time RAKE RECEIVER ANTENNA ADC 8 channels, 10msps
    Contextual Info: Radio Receiver Architectures: Trends for Infrastructure including the Software Radio Design Analog Devices, Inc. January 1999 a Receiver Topics • Introduction: ADI Goals for RX Solutions – Traditional RX Architecture – Technology Trends • IF-Sampling Receivers


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    IS-136 096Mcps IS-136, IS-95, IS136, IS-95 blocking oscillator superheterodyne transceiver UMTS beamforming transceiver rf wcdma rake receiver sample IS-95 mux space time RAKE RECEIVER ANTENNA ADC 8 channels, 10msps PDF

    M2.5 torque settings

    Abstract: ADIS16375 CLM-112-02 DB10 ML-24-3 troubleshooting conditioning circuit for accelerometers Accelerometer filter inertial sensor
    Contextual Info: Low Profile, Low Noise Six Degrees of Freedom Inertial Sensor ADIS16375 Triaxis digital gyroscope, ±300°/sec Tight orthogonal alignment: 0.05° Triaxis digital accelerometer: ±18 g Delta-angle/velocity calculations Wide sensor bandwidth: 330 Hz High sample rate: 2.460 kSPS


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    ADIS16375 10-20-2010-B 24-Lead ML-24-6) ADIS16375AMLZ ADIS16375/PCBZ ML-24-6 M2.5 torque settings ADIS16375 CLM-112-02 DB10 ML-24-3 troubleshooting conditioning circuit for accelerometers Accelerometer filter inertial sensor PDF

    IMU gy 88

    Abstract: IMU gy 86
    Contextual Info: Tactical Grade, Six Degrees of Freedom Inertial Sensor ADIS16485 Data Sheet FEATURES GENERAL DESCRIPTION Triaxial, digital gyroscope, ±450°/sec dynamic range <±0.05° orthogonal alignment 6°/hr in-run bias stability 0.3°/√hr angular random walk 0.01% nonlinearity


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    ADIS16485 ADIS16485 ADIS16485AMLZ ADIS16485/PCBZ 24-Lead ML-24-6 ADIS16485/PCBZ IMU gy 88 IMU gy 86 PDF

    Contextual Info: Low Profile, Low Noise Six Degrees of Freedom Inertial Sensor ADIS16375 Triaxis digital gyroscope, ±300°/sec Tight orthogonal alignment: 0.05° Triaxis digital accelerometer: ±18 g Delta-angle/velocity calculations Wide sensor bandwidth: 330 Hz High sample rate: 2.460 kSPS


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    ADIS16375 10-20-2010-B 24-Lead ML-24-6) ADIS16375AMLZ ADIS16375/PCBZ ML-24-6 D09389-0-7/11 PDF

    Accelerometer filter

    Contextual Info: Low Profile, Low Noise Six Degrees of Freedom Inertial Sensor ADIS16375 Triaxis digital gyroscope, ±300°/sec Tight orthogonal alignment: 0.05° Triaxis digital accelerometer: ±18 g Delta-angle/velocity calculations Wide sensor bandwidth: 330 Hz High sample rate: 2.460 kSPS


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    ADIS16375 10-20-2010-B 24-Lead ML-24-6) ADIS16375AMLZ ADIS16375/PCBZ ML-24-6 ADIS16375 D09389-0-7/11 Accelerometer filter PDF

    Contextual Info: Tactical Grade, Six Degrees of Freedom Inertial Sensor ADIS16485 Data Sheet FEATURES GENERAL DESCRIPTION Triaxial, digital gyroscope, ±450°/sec dynamic range ±0.05° orthogonal alignment error 6°/hr in-run bias stability 0.3°/√hr angular random walk


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    ADIS16485 12-07-2012-E 24-Lead ML-24-6) ADIS16485BMLZ D10666-0-2/15 ML-24-6 PDF

    Contextual Info: Tactical Grade, Six Degrees of Freedom Inertial Sensor ADIS16485 Data Sheet FEATURES GENERAL DESCRIPTION Triaxial, digital gyroscope, ±450°/sec dynamic range <±0.05° orthogonal alignment error 6°/hr in-run bias stability 0.3°/√hr angular random walk


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    ADIS16485 indicato14 12-07-2012-E 24-Lead ML-24-6) ADIS16485AMLZ ML-24-6 D10666-0-4/14 PDF

    Contextual Info: Tactical Grade, Six Degrees of Freedom Inertial Sensor ADIS16485 Data Sheet FEATURES GENERAL DESCRIPTION Triaxial, digital gyroscope, ±450°/sec dynamic range <±0.05° orthogonal alignment error 6°/hr in-run bias stability 0.3°/√hr angular random walk


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    ADIS16485 indicato14 12-07-2012-E 24-Lead ML-24-6) ADIS16485AMLZ ML-24-6 D10666-0-5/14 PDF

    IMU gy 88

    Abstract: troubleshooting conditioning circuit for accelerometers IMU gy 86 Troubleshooting from analog accelerometers inertial sensor IMU gyro 660-4 0x8b00
    Contextual Info: Tactical Grade, Six Degrees of Freedom Inertial Sensor ADIS16485 Data Sheet FEATURES GENERAL DESCRIPTION Triaxial, digital gyroscope, ±450°/sec dynamic range <±0.05° orthogonal alignment 6°/hr in-run bias stability 0.3°/√hr angular random walk 0.01% nonlinearity


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    ADIS16485 ADIS16485 es946 03-28-2012-C 24-Lead ML-24-6) ADIS16485AMLZ ADIS16485/PCBZ IMU gy 88 troubleshooting conditioning circuit for accelerometers IMU gy 86 Troubleshooting from analog accelerometers inertial sensor IMU gyro 660-4 0x8b00 PDF

    IMU gy 86

    Abstract: IMU gyro
    Contextual Info: Tactical Grade, Six Degrees of Freedom Inertial Sensor ADIS16485 Data Sheet FEATURES GENERAL DESCRIPTION Triaxial, digital gyroscope, ±450°/sec dynamic range <±0.05° orthogonal alignment 6°/hr in-run bias stability 0.3°/√hr angular random walk 0.01% nonlinearity


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    ADIS16485 03-28-2012-C 24-Lead ML-24-6) ADIS16485AMLZ ADIS16485/PCBZ ADIS16485/PCBZ ADIS16485AMLZ D10666-0-5/12 IMU gy 86 IMU gyro PDF

    10666-008

    Contextual Info: Tactical Grade, Six Degrees of Freedom Inertial Sensor ADIS16485 Data Sheet FEATURES GENERAL DESCRIPTION Triaxial, digital gyroscope, ±450°/sec dynamic range <±0.05° orthogonal alignment 6°/hr in-run bias stability 0.3°/√hr angular random walk 0.01% nonlinearity


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    ADIS16485 12-07-2012-E 24-Lead ML-24-6) ADIS16485AMLZ ML-24-6 10666-008 PDF

    PID controller equation

    Abstract: 0x000021 implementing FIR and IIR digital filters F12-F0 ADSP filter algorithm implementation ADI90 digital filter ADSP-21000 analog delay line CORE i3 ARCHITECTURE
    Contextual Info: FIR & IIR Filters 4 Digital filtering algorithms are widely used in DSP-based applications, including but not limited to • Audio processing • Speech compression • Modems • Motor control • Video and image processing Historically, electronics designers implemented filters with analog


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    ADI90] ADSP-2100 PID controller equation 0x000021 implementing FIR and IIR digital filters F12-F0 ADSP filter algorithm implementation ADI90 digital filter ADSP-21000 analog delay line CORE i3 ARCHITECTURE PDF

    MEMS ACCELEROMETER 3 axis analog output 10 Khz

    Abstract: ADIS16488AMLZ
    Contextual Info: Tactical Grade Ten Degrees of Freedom Inertial Sensor ADIS16488 Data Sheet FEATURES GENERAL DESCRIPTION Triaxial, digital gyroscope, ±450°/sec dynamic range <±0.05° orthogonal alignment 6°/hr in-run bias stability 0.3°/√hr angular random walk 0.01% nonlinearity


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    ADIS16488 ADIS16488 24-Lead ML-24-6) ADIS16488AMLZ ADIS16488/PCBZ ML-24-6 MEMS ACCELEROMETER 3 axis analog output 10 Khz PDF

    Contextual Info: Tactical Grade Ten Degrees of Freedom Inertial Sensor ADIS16488 Data Sheet FEATURES GENERAL DESCRIPTION Triaxial, digital gyroscope, ±450°/sec dynamic range <±0.05° orthogonal alignment error 6°/hr in-run bias stability 0.3°/√hr angular random walk


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    ADIS16488 correction14 12-07-2012-E 24-Lead ML-24-6) ADIS16488AMLZ ML-24-6 D10277-0-4/14 PDF

    Contextual Info: Tactical Grade Ten Degrees of Freedom Inertial Sensor ADIS16488 Data Sheet FEATURES GENERAL DESCRIPTION Triaxial, digital gyroscope, ±450°/sec dynamic range <±0.05° orthogonal alignment 6°/hr in-run bias stability 0.3°/√hr angular random walk 0.01% nonlinearity


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    ADIS16488 contr14 12-07-2012-E 24-Lead ML-24-6) ADIS16488AMLZ ML-24-6 D10277-0-1/14 PDF

    IMU gy 88

    Abstract: ADIS16480 extended kalman filter WITH ADIS16480 kalman filter accelerometer attitude heading reference system algorithm based on the Kalman filter estimation with extended kalman filter kalman filter C extended kalman filter speed estimation ekf code speed estimation using ekf
    Contextual Info: Ten Degrees of Freedom Inertial Sensor with Dynamic Orientation Outputs ADIS16480 Data Sheet FEATURES GENERAL DESCRIPTION Dynamic angle outputs Quaternion, Euler, rotation matrix 0.1° pitch, roll and 0.3° (yaw) static accuracy Triaxial, digital gyroscope, ±450°/sec dynamic range


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    ADIS16480 ADIS16480 ADIS16480AMLZ ADIS16480/PCBZ 24-Lead ML-24-6 ADIS16480/PCBZ IMU gy 88 extended kalman filter WITH ADIS16480 kalman filter accelerometer attitude heading reference system algorithm based on the Kalman filter estimation with extended kalman filter kalman filter C extended kalman filter speed estimation ekf code speed estimation using ekf PDF

    Contextual Info: Tactical Grade Ten Degrees of Freedom Inertial Sensor ADIS16488 Data Sheet FEATURES GENERAL DESCRIPTION Triaxial, digital gyroscope, ±450°/sec dynamic range <±0.05° orthogonal alignment 6°/hr in-run bias stability 0.3°/√hr angular random walk 0.01% nonlinearity


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    ADIS16488 ADIS16488AMLZ ADIS16488/PCBZ 24-Lead ADIS16488/PCBZ ADIS16488AMLZ ML-24-6 PDF

    dsp lsb modulation demodulation

    Abstract: 16-tap fir filter HP 1001 P2101
    Contextual Info: Conference Paper Improving Fixed-Point DSP Processor System Performance with PLDs as a DSP Coprocessor This presentation gives a general overview of DSP implementation in programmable logic, describes filtering implementations in programmable logic and indicates the techniques and methodology needed to off-load functions


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    ADSP-2100 dsp lsb modulation demodulation 16-tap fir filter HP 1001 P2101 PDF

    difference between harvard architecture super harvard architecture and von neumann block diagram

    Abstract: adsp 21xx processor advantages ADSP21XX FFT CALCULATION adsp 21xx addressing mode addressing modes in adsp-21xx matlab code using 8 point DFT butterfly ADSP-TS001 FIR CODE FOR 8051 IN ASSEMBLY LANGUAGE automatic changeover switch circuit diagram for generator 333MIPS
    Contextual Info: DSP HARDWARE SECTION 7 DSP HARDWARE • Microcontrollers, Microprocessors, and Digital Signal Processors DSPs ■ DSP Requirements ■ ADSP-21xx 16-Bit Fixed-Point DSP Core ■ Fixed-Point Versus Floating Point ■ ADI SHARC Floating Point DSPs ■ ADSP-2116x Single-Instruction, Multiple Data (SIMD)


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    ADSP-21xx 16-Bit ADSP-2116x ADSP-TS001 ADSP-2100 ADSP-2106x difference between harvard architecture super harvard architecture and von neumann block diagram adsp 21xx processor advantages ADSP21XX FFT CALCULATION adsp 21xx addressing mode addressing modes in adsp-21xx matlab code using 8 point DFT butterfly ADSP-TS001 FIR CODE FOR 8051 IN ASSEMBLY LANGUAGE automatic changeover switch circuit diagram for generator 333MIPS PDF

    ys32

    Abstract: ACCELEROMETER using CIRCUIT Troubleshooting from analog accelerometers "Pressure Sensor" magnetometer magnetometer digital barometer sensor ADIS16488 0x8204
    Contextual Info: Tactical Grade Ten Degrees of Freedom Inertial Sensor ADIS16488 Data Sheet FEATURES GENERAL DESCRIPTION Triaxial, digital gyroscope, ±450°/sec dynamic range <±0.05° orthogonal alignment 6°/hr in-run bias stability 0.3°/√hr angular random walk 0.01% nonlinearity


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    ADIS16488 ADIS16488 inertia488AMLZ ADIS16488/PCBZ 24-Lead ML-24-6 ADIS16488/PCBZ ADIS16488AMLZ ys32 ACCELEROMETER using CIRCUIT Troubleshooting from analog accelerometers "Pressure Sensor" magnetometer magnetometer digital barometer sensor 0x8204 PDF

    Contextual Info: Ten Degrees of Freedom Inertial Sensor with Dynamic Orientation Outputs ADIS16480 Data Sheet FEATURES GENERAL DESCRIPTION Dynamic angle outputs Quaternion, Euler, rotation matrix 0.1° pitch, roll and 0.3° (yaw) static accuracy Triaxial, digital gyroscope, ±450°/sec dynamic range


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    ADIS16480 levels14 12-07-2012-E 24-Lead ML-24-6) ADIS16480AMLZ ML-24-6 D10278-0-4/14 PDF

    Contextual Info: Ten Degrees of Freedom Inertial Sensor with Dynamic Orientation Outputs ADIS16480 Data Sheet FEATURES GENERAL DESCRIPTION Dynamic angle outputs Quaternion, Euler, rotation matrix 0.1° pitch, roll and 0.3° (yaw) static accuracy Triaxial, digital gyroscope, ±450°/sec dynamic range


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    ADIS16480 Conf14 12-07-2012-E 24-Lead ML-24-6) ADIS16480AMLZ ML-24-6 D10278-0-1/14 PDF

    xilinx FPGA IIR Filter

    Abstract: PQ208C xilinx logicore fifo generator 6.2 FPGA implementation of IIR Filter digital volume control AD27 AD29 AD30 FPGA based implementation of fixed point IIR Filter Xilinx XC4000 PCMCIA
    Contextual Info: Fall 1996 Seminar LogiCoreTM Solutions LogiCore is a trademark of Xilinx Inc. Fall Seminars - LogiCore - 1 LogiCore Solutions Introduction LogiCore PCI - FPGA Industry’s Most Successful Core FPGA Based DSP - It’s About Time Reference Designs Fall Seminars - LogiCore - 2


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    PDF

    Contextual Info: Tactical Grade Ten Degrees of Freedom Inertial Sensor ADIS16488A Data Sheet FEATURES GENERAL DESCRIPTION Triaxial, digital gyroscope, ±450°/sec dynamic range <±0.05° orthogonal alignment error 5.1°/hr in-run bias stability 0.26°/√hr angular random walk


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    ADIS16488A correc12-07-2012-E 24-Lead ML-24-6) ADIS16488BMLZ ADIS16488CMLZ ML-24-6 PDF