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Name: A40MX04-3PLG44I
Brand: Microchip Technology
SKU: A40MX04-3PLG44I
Price: 2.40 USD
Availability: InStock
Rating: 5 (2 reviews)

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Microchip Technology A40MX04-3PLG44I

Part No.:: A40MX04-3PLG44I

Manufacturer:: Microchip Technology

Package:: 44-LCC (J-Lead)

Datasheet:: A40MX04-3PLG44I.pdf

Description:: IC FPGA 34 I/O 44PLCC

In Stock:: 3771

Quantity:: Add To Cart

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A40MX04-3PLG44I Specifications

Package/Case:
44-LCC (J-Lead)
Packaging:
Tray
Series:
MX
ProductStatus:
Active
NumberofLABs/CLBs:
-
NumberofLogicElements/Cells:
-
TotalRAMBits:
-
NumberofI/O:
34
NumberofGates:
6000
Voltage-Supply:
3V ~ 3.6V, 4.5V ~ 5.5V
MountingType:
Surface Mount
OperatingTemperature:
-40°C ~ 85°C (TA)

A40MX04-3PLG44I this integrated circuit is available in factory sealed anti static packs. at icwhale.com. Please read product page below detail information. including A40MX04-3PLG44I 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 A40MX04-3PLG44I 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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A40MX04-3PLG44I information

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A40MX04-3PLG44I application case analysis in emerging technology fields

A40MX04-3PLG44I is a programmable logic device (PLD) manufactured by Actel Corporation, now part of Microsemi Corporation. It belongs to the A40MX family of FPGAs (Field-Programmable Gate Arrays) and is specifically designed for applications requiring low power consumption and high performance.

Application Scenario:

In the aerospace industry, A40MX04-3PLG44I can be utilized for avionics systems, such as flight control units, navigation systems, and communication modules.

System Design:

To design a flight control unit using A40MX04-3PLG44I, consider the following aspects:

1. Sensor Interface:

Integrate sensors, such as accelerometers, gyroscopes, and altimeters, to provide real-time data on aircraft attitude, velocity, and altitude. Utilize the input/output pins of A40MX04-3PLG44I to interface with these sensors and perform data processing.

2. Control Algorithms:

Implement control algorithms, such as PID (Proportional-Integral-Derivative) controllers, Kalman filters, and state estimation techniques, to stabilize the aircraft and maintain desired flight parameters. Utilize the configurable logic blocks (CLBs) of A40MX04-3PLG44I to execute these algorithms efficiently.

3. Communication:

Establish communication interfaces, such as UART, CAN (Controller Area Network), or Ethernet, for data exchange with other avionics systems and ground control stations. Configure the dedicated I/O pins and serial transceivers of A40MX04-3PLG44I for reliable data transmission.

4. Redundancy and Fault Tolerance:

Implement redundancy and fault-tolerant mechanisms to ensure the reliability and safety of the flight control system. Utilize the reconfigurable nature of A40MX04-3PLG44I to dynamically adapt to changing operational conditions and mitigate single points of failure.

5. Power Management:

Optimize power consumption by employing low-power design techniques and dynamic power management schemes. Utilize the standby and sleep modes of A40MX04-3PLG44I to conserve energy during idle periods and extend battery life in battery-powered aircraft.

Considerations:

When designing the flight control unit, it's essential to consider:

- Safety-Critical Design: Ensure compliance with aviation safety standards, such as RTCA/DO-254, and perform thorough verification and validation testing to mitigate risks associated with software and hardware failures.

- Environmental Factors: Consider the operating environment, including temperature variations, humidity levels, and electromagnetic interference, and design the system to withstand harsh conditions encountered during flight.

- Performance Optimization: Employ optimization techniques, such as parallel processing, pipelining, and resource sharing, to maximize the utilization of A40MX04-3PLG44I resources and improve overall system performance.

- Scalability and Upgradability: Design the flight control unit with scalability and upgradability in mind to accommodate future enhancements, such as additional sensors, communication protocols, or advanced control algorithms, without requiring significant hardware modifications.

- Regulatory Compliance: Ensure compliance with regulatory requirements imposed by aviation authorities, such as the Federal Aviation Administration (FAA) in the United States and the European Aviation Safety Agency (EASA) in Europe, to obtain certification for the flight control system.

A40MX04-3PLG44I FAQ

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3. Are the A40MX04-3PLG44I price and inventory displayed accurate?

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6. What is the process for return or replacement of A40MX04-3PLG44I?

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 A40MX04-3PLG44I we delivered, we will accept the replacement or return of the A40MX04-3PLG44I 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 A40MX04-3PLG44I.

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

Two processes to return the products:

(1)Inform us within 90 days

(2)Obtain Requesting Return Authorizations