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Name: A40MX04-1PLG68I
Brand: Microchip Technology
SKU: A40MX04-1PLG68I
Price: 2.40 USD
Availability: InStock
Rating: 5 (2 reviews)

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Microchip Technology A40MX04-1PLG68I

Part No.:: A40MX04-1PLG68I

Manufacturer:: Microchip Technology

Package:: 68-LCC (J-Lead)

Datasheet:: A40MX04-1PLG68I.pdf

Description:: IC FPGA 57 I/O 68PLCC

In Stock:: 2464

Quantity:: Add To Cart

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A40MX04-1PLG68I Specifications

Package/Case:
68-LCC (J-Lead)
Packaging:
Tray
Series:
MX
ProductStatus:
Active
NumberofLABs/CLBs:
-
NumberofLogicElements/Cells:
-
TotalRAMBits:
-
NumberofI/O:
57
NumberofGates:
6000
Voltage-Supply:
3V ~ 3.6V, 4.5V ~ 5.5V
MountingType:
Surface Mount
OperatingTemperature:
-40°C ~ 85°C (TA)

A40MX04-1PLG68I this integrated circuit is available in factory sealed anti static packs. at icwhale.com. Please read product page below detail information. including A40MX04-1PLG68I price, data-sheet, in-stock availability, technical difficulties. Also. Quickly Enter the access of compare listing to find out replaceable electronic parts. If you want to retrieve comprehensive data for A40MX04-1PLG68I to optimize the supply chain (including cross references, life-cycle, parametric, counterfeit risk, obsolescence managements forecasts), please contact to our Tech-supports team.

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A40MX04-1PLG68I information

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A40MX04-1PLG68I application case analysis in emerging technology fields

A40MX04-1PLG68I is a field-programmable gate array (FPGA) device manufactured by Actel Corporation, offering flexibility and customization for a wide range of applications. With its 40,000 system gates, this FPGA provides ample resources for implementing complex logic functions and interfaces.

Application Scenario:

In the aerospace industry, A40MX04-1PLG68I can be utilized in avionics systems to enhance performance and reliability. Let's explore how it can be applied in the context of flight control systems.

Flight Control System Design:

To design an efficient and intelligent flight control system using A40MX04-1PLG68I, the following steps can be followed:

1. Sensor Interface:

Integrate sensors such as accelerometers, gyroscopes, and altimeters to capture real-time flight data. Connect these sensors to the input pins of A40MX04-1PLG68I for processing and analysis.

2. Control Logic:

Implement control algorithms and logic functions within the FPGA to process sensor data and generate control signals for various flight control surfaces, including ailerons, elevators, and rudders.

3. Redundancy and Fault Tolerance:

Utilize the reconfigurable nature of A40MX04-1PLG68I to implement redundant control paths and fault-tolerant mechanisms. This ensures continued operation in the event of sensor failures or other system faults.

4. Communication:

Establish communication interfaces, such as CAN (Controller Area Network) or Ethernet, to facilitate data exchange with other avionics systems, ground control stations, or satellite communication systems. Configure the appropriate FPGA pins for serial communication protocols.

5. Real-Time Processing:

Implement efficient firmware algorithms and hardware acceleration techniques within A40MX04-1PLG68I to enable real-time processing of sensor data and generation of control signals with minimal latency. This ensures responsive and precise flight control.

Considerations:

When designing the flight control system using A40MX04-1PLG68I, it's essential to consider:

- Resource Utilization: Optimize the utilization of FPGA resources to accommodate the required logic functions and interfaces while minimizing resource conflicts.

- Power Efficiency: Implement power-saving techniques such as clock gating and dynamic voltage scaling to minimize power consumption and extend battery life in battery-powered applications.

- Environmental Conditions: Ensure that the FPGA and associated components are designed to withstand the harsh environmental conditions encountered in aerospace applications, including temperature variations, humidity, and vibration.

- Regulatory Compliance: Ensure compliance with aviation regulatory standards, such as RTCA DO-254 for hardware development and DO-178C for software development, to ensure the safety and airworthiness of the flight control system.

- Testing and Validation: Thoroughly test the flight control system, including hardware-in-the-loop (HIL) simulation and flight testing, to verify performance, reliability, and safety before deployment in actual aircraft.

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6. What is the process for return or replacement of A40MX04-1PLG68I?

All goods will implement Pre-Shipment Inspection (PSI), selected at random from all batches of your order to do a systematic inspection before arranging the shipment. If there is something wrong with the A40MX04-1PLG68I we delivered, we will accept the replacement or return of the A40MX04-1PLG68I only when all of the below conditions are fulfilled:

(1)Such as a deficiency in quantity, delivery of wrong items, and apparent external defects (breakage and rust, etc.), and we acknowledge such problems.

(2)We are informed of the defect described above within 90 days after the delivery of A40MX04-1PLG68I.

(3)The PartNo is unused and only in the original unpacked packaging.

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(1)Inform us within 90 days

(2)Obtain Requesting Return Authorizations