ZHCSJA4B January   2019  – May 2022 DLP4500

PRODUCTION DATA  

  1. 特性
  2. 应用
  3. 说明
  4. Revision History
  5. Chipset Component Usage Specification
  6. Pin Configuration and Functions
  7. Specifications
    1. 7.1  Absolute Maximum Ratings
    2. 7.2  Storage Conditions
    3. 7.3  ESD Ratings
    4. 7.4  Recommended Operating Conditions
    5. 7.5  Thermal Information
    6. 7.6  Electrical Characteristics
    7. 7.7  Timing Requirements
    8. 7.8  System Mounting Interface Loads
    9. 7.9  Micromirror Array Physical Characteristics
    10. 7.10 Micromirror Array Optical Characteristics
    11. 7.11 Typical Characteristics
  8. Detailed Description
    1. 8.1 Overview
    2. 8.2 Functional Block Diagram
    3. 8.3 Feature Description
    4. 8.4 Device Functional Modes
      1. 8.4.1 Operating Modes
    5. 8.5 Micromirror Array Temperature Calculation
      1. 8.5.1 Package Thermal Resistance
      2. 8.5.2 Case Temperature
        1. 8.5.2.1 Temperature Calculation
    6. 8.6 Micromirror Landed-on/Landed-Off Duty Cycle
      1. 8.6.1 Definition of Micromirror Landed-On/Landed-Off Duty Cycle
      2. 8.6.2 Landed Duty Cycle and Useful Life of the DMD
      3. 8.6.3 Landed Duty Cycle and Operational DMD Temperature
      4. 8.6.4 Estimating the Long-Term Average Landed Duty Cycle of a Product or Application
  9. Application and Implementation
    1. 9.1 Application Information
    2. 9.2 Typical Application
      1. 9.2.1 Design Requirements
      2. 9.2.2 Detailed Design Procedure
        1. 9.2.2.1 DLPC350 System Interfaces
          1. 9.2.2.1.1 Control Interface
          2. 9.2.2.1.2 Input Data Interface
        2. 9.2.2.2 DLPC350 System Output Interfaces
          1. 9.2.2.2.1 Illumination Interface
          2. 9.2.2.2.2 Trigger Interface (Sync Outputs)
        3. 9.2.2.3 DLPC350 System Support Interfaces
          1. 9.2.2.3.1 Reference Clock
          2. 9.2.2.3.2 PLL
          3. 9.2.2.3.3 Program Memory Flash Interface
        4. 9.2.2.4 DMD Interfaces
          1. 9.2.2.4.1 DLPC350 to DMD Digital Data
          2. 9.2.2.4.2 DLPC350 to DMD Control Interface
          3. 9.2.2.4.3 DLPC350 to DMD Micromirror Reset Control Interface
  10. 10Power Supply Recommendations
    1. 10.1 Power Supply Sequencing Requirements
    2. 10.2 DMD Power Supply Power-Up Procedure
    3. 10.3 DMD Power Supply Power-Down Procedure
  11. 11Layout
    1. 11.1 Layout Guidelines
      1. 11.1.1 DMD Interface Design Considerations
      2. 11.1.2 DMD Termination Requirements
      3. 11.1.3 Decoupling Capacitors
      4. 11.1.4 Power Plane Recommendations
      5. 11.1.5 Signal Layer Recommendations
      6. 11.1.6 General Handling Guidelines for CMOS-Type Pins
      7. 11.1.7 PCB Manufacturing
        1. 11.1.7.1 General Guidelines
        2. 11.1.7.2 Trace Widths and Minimum Spacings
        3. 11.1.7.3 Routing Constraints
        4. 11.1.7.4 Fiducials
        5. 11.1.7.5 Flex Considerations
        6. 11.1.7.6 DLPC350 Thermal Considerations
    2. 11.2 Layout Example
      1. 11.2.1 Printed Circuit Board Layer Stackup Geometry
      2. 11.2.2 Recommended DLPC350 MOSC Crystal Oscillator Configuration
      3. 11.2.3 Recommended DLPC350 PLL Layout Configuration
  12. 12Device and Documentation Support
    1. 12.1 Device Support
      1. 12.1.1 第三方产品免责声明
      2. 12.1.2 Device Nomenclature
    2. 12.2 Device Markings
    3. 12.3 Documentation Support
      1. 12.3.1 Related Documentation
    4. 12.4 接收文档更新通知
    5. 12.5 支持资源
    6.     Trademarks
    7. 12.6 Electrostatic Discharge Caution
    8. 12.7 术语表
  13. 13Mechanical, Packaging, and Orderable Information

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订购信息

Estimating the Long-Term Average Landed Duty Cycle of a Product or Application

During a given period of time, the landed duty cycle of a given micromirror follows from the image content being displayed by that micromirror.

For example, in the simplest case, when displaying pure-white on a given micromirror for a given time period, that micromirror experiences a 100/0 landed duty cycle during that time period. Likewise, when displaying pure-black, the micromirror experiences a 0/100 landed duty cycle.

Between the two extremes (ignoring for the moment color and any image processing that may be applied to an incoming image), the landed duty cycle tracks one-to-one with the linear gray scale value, as shown in Table 8-2.

Table 8-2 Grayscale Value and Landed Duty Cycle
GRAYSCALE VALUE NOMINAL LANDED DUTY CYCLE
0% 0/100
10% 10/90
20% 20/80
30% 30/70
40% 40/60
50% 50/50
60% 60/40
70% 70/30
80% 80/20
90% 90/10
100% 100/0

Accounting for color rendition (but still ignoring image processing) requires knowing both the color intensity (from 0% to 100%) for each constituent primary color (red, green, and/or blue) for the given micromirror as well as the color cycle time for each primary color, where “color cycle time” is the total percentage of the frame time that a given primary must be displayed in order to achieve the desired white point.

During a given period of time, the landed duty cycle of a given micromirror can be calculated as follows:

Equation 6. Landed Duty Cycle = (Red_Cycle_% × Red_Scale_Value) + (Green_Cycle_% × Green_Scale_Value) + (Blue_Cycle_% × Blue_Scale_Value)

where

  • Red_Cycle_%, Green_Cycle_%, and Blue_Cycle_%, represent the percentage of the frame time that Red, Green, and Blue are displayed (respectively) to achieve the desired white point.

For example, assume that the red, green and blue color cycle times are 50%, 20%, and 30% respectively (in order to achieve the desired white point), then the landed duty cycle for various combinations of red, green, blue color intensities would be as shown in Table 8-3.

Table 8-3 Example Landed Duty Cycle for Full-Color
RED CYCLE PERCENTAGE
50%
GREEN CYCLE PERCENTAGE
20%
BLUE CYCLE PERCENTAGE
30%
NOMINAL LANDED DUTY CYCLE
RED SCALE VALUE GREEN SCALE VALUE BLUE SCALE VALUE
0% 0% 0% 0/100
100% 0% 0% 50/50
0% 100% 0% 20/80
0% 0% 100% 30/70
12% 0% 0% 6/94
0% 35% 0% 7/93
0% 0% 60% 18/82
100% 100% 0% 70/30
0% 100% 100% 50/50
100% 0% 100% 80/20
12% 35% 0% 13/87
0% 35% 60% 25/75
12% 0% 60% 24/76
100% 100% 100% 100/0