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Name: M1A3P250-2FGG144I
Brand: Microchip Technology
SKU: M1A3P250-2FGG144I
Price: 2.40 USD
Availability: InStock
Rating: 5 (2 reviews)

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Microchip Technology M1A3P250-2FGG144I

Part No.:: M1A3P250-2FGG144I

Manufacturer:: Microchip Technology

Package:: 144-LBGA

Datasheet:: M1A3P250-2FGG144I.pdf

Description:: IC FPGA 97 I/O 144FBGA

In Stock:: 2573

Quantity:: Add To Cart

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M1A3P250-2FGG144I Specifications

Package/Case:
144-LBGA
Packaging:
Tray
Series:
ProASIC3
ProductStatus:
Active
NumberofLABs/CLBs:
-
NumberofLogicElements/Cells:
-
TotalRAMBits:
36864
NumberofI/O:
97
NumberofGates:
250000
Voltage-Supply:
1.425V ~ 1.575V
MountingType:
Surface Mount
OperatingTemperature:
-40°C ~ 100°C (TJ)

M1A3P250-2FGG144I this integrated circuit is available in factory sealed anti static packs. at icwhale.com. Please read product page below detail information. including M1A3P250-2FGG144I 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 M1A3P250-2FGG144I 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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M1A3P250-2FGG144I information

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M1A3P250-2FGG144I application case analysis in emerging technology fields

M1A3P250-2FGG144I is a high-performance FPGA (Field-Programmable Gate Array) chip designed by Microchip Technology, offering versatility and efficiency for a wide range of applications.

Application Scenario:

In aerospace engineering, M1A3P250-2FGG144I can be utilized to enhance the efficiency and intelligence of avionics systems, such as flight control systems in unmanned aerial vehicles (UAVs).

System Design:

To implement a flight control system using M1A3P250-2FGG144I, consider the following steps:

1. Sensor Integration:

Integrate various sensors, including gyroscopes, accelerometers, and GPS modules, to provide real-time data on the UAV's orientation, velocity, and position. Utilize the configurable I/O pins of M1A3P250-2FGG144I to interface with these sensors efficiently.

2. Control Algorithm:

Develop advanced control algorithms, such as PID (Proportional-Integral-Derivative) controllers or Kalman filters, to stabilize the UAV's flight and ensure smooth navigation. Implement these algorithms using the FPGA's programmable logic resources for fast and precise computation.

3. Actuator Control:

Connect actuators, such as motors and servos, to the FPGA's GPIO pins for controlling the UAV's propulsion, attitude, and altitude. Utilize PWM (Pulse-Width Modulation) signals generated by the FPGA to drive these actuators accurately.

4. Communication Interface:

Implement communication interfaces, such as UART or Ethernet, to facilitate data exchange between the FPGA-based flight control system and ground control stations or other UAV subsystems. Configure the relevant FPGA pins for serial communication and networking protocols.

5. Power Management:

Design efficient power management circuitry to supply the required voltages to M1A3P250-2FGG144I and connected peripherals while optimizing power consumption for extended flight durations. Utilize voltage regulators and power monitoring circuits to ensure stable operation.

Considerations:

When designing the UAV flight control system, consider the following factors:

- Real-Time Processing: Utilize the FPGA's parallel processing capabilities to handle multiple sensor inputs and control outputs simultaneously, ensuring responsive and stable flight control.

- Fault Tolerance: Implement redundancy and error detection mechanisms within the FPGA firmware to mitigate the effects of sensor failures or communication errors, enhancing the system's reliability.

- Environmental Adaptability: Ensure that the FPGA-based flight control system can operate reliably in various environmental conditions, including temperature extremes, humidity, and vibration, by selecting ruggedized components and appropriate enclosure designs.

- Regulatory Compliance: Verify that the UAV flight control system complies with relevant aviation regulations and standards, including safety certifications and electromagnetic compatibility (EMC) requirements, to ensure airworthiness and interoperability with other airspace systems.

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6. What is the process for return or replacement of M1A3P250-2FGG144I?

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 M1A3P250-2FGG144I we delivered, we will accept the replacement or return of the M1A3P250-2FGG144I 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 M1A3P250-2FGG144I.

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

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(1)Inform us within 90 days

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