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Name: XC7VX690T-2FFG1926C
Brand: AMD Xilinx
SKU: XC7VX690T-2FFG1926C
Price: 2.40 USD
Availability: InStock
Rating: 5 (2 reviews)

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AMD Xilinx XC7VX690T-2FFG1926C

Part No.:: XC7VX690T-2FFG1926C

Manufacturer:: AMD Xilinx

Package:: 1924-BBGA, FCBGA

Datasheet:: XC7VX690T-2FFG1926C.pdf

Description:: IC FPGA 720 I/O 1926FCBGA

In Stock:: 2349

Quantity:: Add To Cart

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XC7VX690T-2FFG1926C Specifications

Package/Case:
1924-BBGA, FCBGA
Packaging:
Tray
Series:
Virtex®-7 XT
ProductStatus:
Active
NumberofLABs/CLBs:
54150
NumberofLogicElements/Cells:
693120
TotalRAMBits:
54190080
NumberofI/O:
720
NumberofGates:
-
Voltage-Supply:
0.97V ~ 1.03V
MountingType:
Surface Mount
OperatingTemperature:
0°C ~ 85°C (TJ)

XC7VX690T-2FFG1926C this integrated circuit is available in factory sealed anti static packs. at icwhale.com. Please read product page below detail information. including XC7VX690T-2FFG1926C 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 XC7VX690T-2FFG1926C 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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XC7VX690T-2FFG1926C information

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XC7VX690T-2FFG1926C application case analysis in emerging technology fields

XC7VX690T-2FFG1926C is an FPGA (Field-Programmable Gate Array) device renowned for its exceptional performance and versatility in various high-performance computing applications.

Application Scenario:

In the domain of aerospace engineering, XC7VX690T-2FFG1926C plays a pivotal role in enabling advanced guidance, navigation, and control systems for spacecraft and satellites, ultimately contributing to the exploration of outer space.

System Design:

To design a guidance, navigation, and control system utilizing XC7VX690T-2FFG1926C, the following steps are crucial:

1. Sensor Integration:

Utilize high-precision sensors such as accelerometers, gyroscopes, and magnetometers to gather real-time data on spacecraft orientation, motion, and environmental conditions. Interface these sensors with XC7VX690T-2FFG1926C through appropriate analog or digital interfaces for data acquisition.

2. Algorithm Implementation:

Develop and implement complex algorithms for attitude determination, trajectory calculation, and maneuver planning using the computational power of XC7VX690T-2FFG1926C. These algorithms should be optimized for efficient execution on the FPGA architecture to ensure real-time responsiveness and accuracy.

3. Control Logic:

Design and deploy control logic modules within XC7VX690T-2FFG1926C to regulate spacecraft attitude, trajectory, and propulsion systems. Implement closed-loop control algorithms to maintain desired navigation objectives and respond to dynamic environmental conditions.

4. Redundancy and Fault Tolerance:

Implement redundancy schemes and fault-tolerant mechanisms within the FPGA design to ensure system reliability and resilience against potential hardware failures or radiation-induced errors encountered in the harsh space environment.

5. Communication Interface:

Integrate communication interfaces, such as SpaceWire or Ethernet, into the XC7VX690T-2FFG1926C system to facilitate data exchange with other onboard subsystems, ground stations, or satellite networks. Configure high-speed serial transceivers and protocol stacks for reliable data transmission.

Considerations:

When designing the guidance, navigation, and control system with XC7VX690T-2FFG1926C, it's essential to address the following considerations:

- Radiation Hardening: Implement radiation-hardening techniques to mitigate the effects of ionizing radiation on FPGA operation and maintain system integrity in space.

- Power Efficiency: Optimize FPGA configurations and algorithm implementations for power efficiency to prolong the spacecraft's operational lifespan and minimize energy consumption.

- Thermal Management: Employ thermal management strategies to dissipate heat generated by XC7VX690T-2FFG1926C and ensure reliable performance over extended mission durations.

- Verification and Validation: Conduct rigorous testing, simulation, and verification procedures to validate the functionality, performance, and safety of the guidance, navigation, and control system prior to deployment in space missions.

- Scalability and Flexibility: Design the FPGA-based system with scalability and flexibility in mind to accommodate future upgrades, mission adaptations, and evolving mission requirements in the dynamic space exploration landscape.

XC7VX690T-2FFG1926C FAQ

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6. What is the process for return or replacement of XC7VX690T-2FFG1926C?

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 XC7VX690T-2FFG1926C we delivered, we will accept the replacement or return of the XC7VX690T-2FFG1926C 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 XC7VX690T-2FFG1926C.

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

Two processes to return the products:

(1)Inform us within 90 days

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