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Name: A3PE600-FGG484
Brand: Microchip Technology
SKU: A3PE600-FGG484
Price: 2.40 USD
Availability: InStock
Rating: 5 (2 reviews)

Any Feature, including a modified Existing Feature, that is not an Existing Feature.

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Microchip Technology A3PE600-FGG484

Part No.:: A3PE600-FGG484

Manufacturer:: Microchip Technology

Package:: 484-BGA

Datasheet:: A3PE600-FGG484.pdf

Description:: IC FPGA 270 I/O 484FBGA

In Stock:: 2627

Quantity:: Add To Cart

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A3PE600-FGG484 Specifications

Package/Case:
484-BGA
Packaging:
Tray
Series:
ProASIC3E
ProductStatus:
Active
NumberofLABs/CLBs:
-
NumberofLogicElements/Cells:
-
TotalRAMBits:
110592
NumberofI/O:
270
NumberofGates:
600000
Voltage-Supply:
1.425V ~ 1.575V
MountingType:
Surface Mount
OperatingTemperature:
0°C ~ 85°C (TJ)

A3PE600-FGG484 this integrated circuit is available in factory sealed anti static packs. at icwhale.com. Please read product page below detail information. including A3PE600-FGG484 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 A3PE600-FGG484 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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A3PE600-FGG484 information

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A3PE600-FGG484 application case analysis in emerging technology fields

A3PE600-FGG484 is a Field-Programmable Gate Array (FPGA) device manufactured by Microsemi Corporation. It offers high logic capacity, versatile I/O capabilities, and robust performance, making it suitable for a wide range of applications in various industries.

Application Scenario:

In the aerospace industry, A3PE600-FGG484 can be utilized for avionics systems, such as flight control systems in unmanned aerial vehicles (UAVs).

System Design:

To design a flight control system using A3PE600-FGG484, follow these steps:

1. Sensor Integration:

Integrate sensors, such as accelerometers, gyroscopes, and GPS receivers, to gather real-time data about the UAV's orientation, position, and velocity. Interface these sensors with A3PE600-FGG484 using appropriate communication protocols, such as SPI or I2C.

2. Control Algorithm Implementation:

Develop control algorithms, such as PID (Proportional-Integral-Derivative) controllers or state estimation filters, to stabilize the UAV's flight and navigate it to desired waypoints. Implement these algorithms in the FPGA fabric of A3PE600-FGG484 to achieve low-latency and high-throughput processing.

3. Actuator Control:

Connect actuators, such as motors or servos, to the output pins of A3PE600-FGG484 to control the UAV's propulsion, attitude, and altitude. Utilize PWM (Pulse-Width Modulation) signals generated by the FPGA to precisely regulate the speed and position of the actuators.

4. Communication Interface:

Implement communication interfaces, such as UART or Ethernet, to communicate with ground control stations or other UAVs in the network. Utilize the high-speed transceivers available in A3PE600-FGG484 for reliable data transmission over long distances.

5. Power Management:

Ensure efficient power supply and distribution within the UAV system to meet the power requirements of A3PE600-FGG484 and other onboard components. Incorporate voltage regulators, power converters, and battery management systems to maintain stable operation throughout the flight duration.

Considerations:

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

- Safety Redundancy: Implement redundant sensors, actuators, and communication links to ensure safe operation in case of component failures.

- Environmental Conditions: Design the system to withstand harsh environmental conditions, such as temperature extremes, humidity, and vibration, commonly encountered during UAV operations.

- Regulatory Compliance: Ensure that the flight control system complies with aviation regulations and standards, such as those set forth by the Federal Aviation Administration (FAA) or the European Union Aviation Safety Agency (EASA).

- Real-Time Performance: Optimize the FPGA firmware and hardware design for real-time processing to maintain precise control over the UAV's flight dynamics and response to external stimuli.

- System Integration: Test the complete UAV system thoroughly to verify interoperability and performance across all subsystems, including the A3PE600-FGG484-based flight control module.

A3PE600-FGG484 FAQ

1. How to order A3PE600-FGG484 on icwhale.com?

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3. Are the A3PE600-FGG484 price and inventory displayed accurate?

The price and inventory of A3PE600-FGG484 fluctuates frequently and cannot be updated in time, it will be updated periodically within 24 hours. And, our quotation usually expires after 5 days.

4. What forms of payment are accepted?

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5. How is the shipping arranged?

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Once your order has been processed for shipment, our salesperson will send you an email advising you of the shipping status and tracking number.

Warm Tips: It may take up to 24 hours for the carriers to display tracking information. Usually, express delivery takes 3-5 days, and registered mail takes 25-60 days.

6. What is the process for return or replacement of A3PE600-FGG484?

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 A3PE600-FGG484 we delivered, we will accept the replacement or return of the A3PE600-FGG484 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 A3PE600-FGG484.

(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