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DRV8308 Ensure safe implementation in airborne systems

DO-254/ED-80 defines two categories of hardware items.

• Complex electronic hardware.

• Simple electronic hardware.

All flight hardware needs to be classified according to a design assurance level (DAL). The standard defines five levels regarding the safety and criticality of an avionic system (A to E).

Does this 3-Phase BLDC Motor Pre-Driver with Integrated Speed Control and Commutation Logic fall into either of these two categories?

The end use for our application for a system failure is level C

Level C: The SEH associated with functions whose failure or malfunction could cause a major failure condition as determined by the system safety assessment (design assurance level C hardware) should undergo a comprehensive combination of deterministic testing and analysis that demonstrates correct operation under all possible combinations and permutations of conditions of the inputs at the pins of the device (i.e., those inputs available external to the packaging of the device). All possible states of any sequential state machines should also be tested.

  • Hi John,

    We will check and get back to you. By you question, are there categories other than complex or simple electronic hardware?
  • I'm not expert on the DO-254 requirements, but these are two categories defined within the specification.
    Appendix C of DO-254/ED-80 defines a simple hardware item as the following:

    Simple Hardware Item – A hardware item is considered simple if a comprehensive combination of deterministic tests and analyses can ensure correct functional performance under all foreseeable operating conditions with no anomalous behavior.

    Complex Hardware Item – All items that are not simple are considered to be complex. See definition of Simple Hardware Item.

    Is the motor controller a custom micro-coded component? Programmable Logic Device (PLD), Application Specific Integrated Circuit (ASIC) - Integrated Circuits which are developed to implement a function, including, but not limited to: gate arrays, standard cells and full custom components encompassing linear, digital and mixed mode technologies.

    How has TI addressed using this component in aerospace application and is fault free of potentially hidden states in sequential machines?