SLOSEB6D February   2025  – November 2025 LMH13000

PRODUCTION DATA  

  1.   1
  2. Features
  3. Applications
  4. Description
  5. Pin Configuration and Functions
  6. Specifications
    1. 5.1 Absolute Maximum Ratings
    2. 5.2 ESD Ratings
    3. 5.3 Recommended Operating Conditions
    4. 5.4 Thermal Information
    5. 5.5 Electrical Characteristics for Low-Current Mode, MODE = 0
    6. 5.6 Electrical Characteristics for High-Current Mode, MODE = 1
    7. 5.7 Typical Characteristics
    8. 5.8 Parameter Measurement Information
  7. Detailed Description
    1. 6.1 Overview
    2. 6.2 Functional Block Diagram
    3. 6.3 Feature Description
      1. 6.3.1 Constant Current (ICC)
      2. 6.3.2 Propagation Delay With Temperature
        1. 6.3.2.1 Calibration of Propagation Delay With Temperature
        2. 6.3.2.2 Start Pulse Directly From IOUT
    4. 6.4 Device Functional Modes
  8. Application and Implementation
    1. 7.1 Application Information
    2. 7.2 Typical Application
      1. 7.2.1 Optical Time-of-Flight System
        1. 7.2.1.1 Design Requirements
        2. 7.2.1.2 Detailed Design Procedure
        3. 7.2.1.3 Application Curve
      2. 7.2.2 Automatic Power-Control Loop Using the LMH13000
    3. 7.3 Power Supply Recommendations
    4. 7.4 Layout
      1. 7.4.1 Layout Guidelines
      2. 7.4.2 Layout Example
  9. Device and Documentation Support
    1. 8.1 Receiving Notification of Documentation Updates
    2. 8.2 Support Resources
    3. 8.3 Trademarks
    4. 8.4 Electrostatic Discharge Caution
    5. 8.5 Glossary
  10. Revision History
  11. 10Mechanical, Packaging, and Orderable Information

Calibration of Propagation Delay With Temperature

Systems that rely on LVDS input to the LMH13000 as the start reference point for time-of-flight calculations require accurate calibration of the prorogation delay from LVDS to IOUT. Propagation delay varies with temperature as a result of changes in device behavior, thus creating timing mismatches in sensitive systems.

Measurement and Calibration Approach:

  1. Measure propagation delay values at three key temperature points: low (-40°C), ambient (25°C), and high (125°C).
  2. A second-order polynomial fit is applied to the delay versus temperature curve using linear regression techniques.
  3. Use this polynomial equation to predict delay values at intermediate temperatures.
  4. See Figure 5-30 for error in delay estimation. The graph shows the difference between actual measured delay versus predicted delay.

This calibration technique enables effective compensation for temperature-induced propagation delay shifts. Applying the polynomial correction maintains consistent timing behavior across operating conditions.