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Name: EP2S30F484I4N
Brand: Intel
SKU: EP2S30F484I4N
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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Intel EP2S30F484I4N

Part No.:: EP2S30F484I4N

Manufacturer:: Intel

Package:: 484-BBGA

Datasheet:: EP2S30F484I4N.pdf

Description:: IC FPGA 342 I/O 484FBGA

In Stock:: 3752

Quantity:: Add To Cart

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EP2S30F484I4N Specifications

Package/Case:
484-BBGA
Packaging:
Tray
Series:
Stratix® II
ProductStatus:
Obsolete
NumberofLABs/CLBs:
1694
NumberofLogicElements/Cells:
33880
TotalRAMBits:
1369728
NumberofI/O:
342
NumberofGates:
-
Voltage-Supply:
1.15V ~ 1.25V
MountingType:
Surface Mount
OperatingTemperature:
-40°C ~ 100°C (TJ)

EP2S30F484I4N this integrated circuit is available in factory sealed anti static packs. at icwhale.com. Please read product page below detail information. including EP2S30F484I4N 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 EP2S30F484I4N 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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EP2S30F484I4N information

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The application and technological advancement of EP2S30F484I4N in specific industries

EP2S30F484I4N is a field-programmable gate array (FPGA) chip known for its versatility and high performance, commonly utilized across various industries for specialized applications. It features a large number of logic elements, embedded memory blocks, and flexible I/O options.

Application Scenario:

In the aerospace industry, EP2S30F484I4N plays a crucial role in the development of avionics systems, specifically in the design and implementation of flight control systems for unmanned aerial vehicles (UAVs).

Circuit Design:

To design a flight control system using EP2S30F484I4N, follow these steps:

1. Sensor Integration:

Integrate various sensors, such as gyroscopes, accelerometers, and GPS modules, to gather real-time flight data. Connect these sensors to the appropriate I/O pins of EP2S30F484I4N for data acquisition and processing.

2. Control Algorithm Implementation:

Develop and implement control algorithms, including PID (Proportional-Integral-Derivative) controllers, Kalman filters, and state estimation algorithms, using the logic elements and embedded memory blocks of EP2S30F484I4N. These algorithms ensure stable and precise flight control.

3. Actuator Interface:

Connect actuators such as motors, servos, and control surfaces to the FPGA's GPIO pins for controlling the UAV's movement based on the output of the control algorithms. Implement PWM (Pulse-Width Modulation) signals or other appropriate control signals to drive these actuators.

4. Communication:

Implement communication interfaces, such as UART, SPI, or Ethernet, to facilitate data exchange between the FPGA-based flight control system and other onboard systems or ground control stations. Configure the relevant I/O pins for serial or parallel communication as required.

5. Redundancy and Safety Measures:

Ensure redundancy and safety features in the design to guarantee the reliability and integrity of the flight control system. Implement fault-tolerant mechanisms, redundant sensor configurations, and watchdog timers to mitigate the risk of system failures.

Considerations:

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

- Performance Optimization: Optimize the FPGA design to minimize resource utilization while maximizing computational efficiency and system responsiveness.

- Environmental Factors: Design the system to withstand harsh environmental conditions encountered during flight, including temperature extremes, vibration, and electromagnetic interference.

- Regulatory Compliance: Ensure that the flight control system complies with aviation regulatory standards and safety guidelines to obtain certification for UAV deployment in commercial or military operations.

- Testing and Validation: Conduct thorough testing and validation of the FPGA-based flight control system through simulation, emulation, and real-world flight testing to verify its functionality, stability, and safety performance.

EP2S30F484I4N FAQ

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3. Are the EP2S30F484I4N price and inventory displayed accurate?

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6. What is the process for return or replacement of EP2S30F484I4N?

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 EP2S30F484I4N we delivered, we will accept the replacement or return of the EP2S30F484I4N 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 EP2S30F484I4N.

(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