// SYS-HW-03 · Avionics

HARDWARE & PROGRAMS

Embedded avionics, flight-computer electronics, sensor interfaces, and custom hardware architectures developed around the requirements of autonomous aerospace platforms.

Embedded compute
High-performance processing architecture for real-time aerospace workloads.
Sensor & vehicle interfaces
Structured connectivity for inertial, navigation, communication, power, and vehicle subsystems.
Program-specific architecture
Component selection, interfaces, protection, and verification are defined around the platform requirement.
Three-quarter view of an illustrative black SWORT Aerospace avionics board with processors, power components, communication interfaces, sensor connectors, headers, and corner mounting holes.
Illustrative representation, not a SWORT printed circuit board. Actual board designs are protected intellectual property and are not publicly displayed. Access is granted only under a non-disclosure agreement approved by the SWORT board.

Interactive architecture

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The interactive model is a visual aid. Equivalent architecture information is provided in the surrounding text.

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// PROGRAM PUBLICATION

Selected programs

Detailed customer programs are published only after technical review and customer authorization. Approved case studies will be added as program material becomes releasable.

Discuss a Program

// SYS-LAB-07 · VERIFICATION

FROM THE LAB

Verification activities are selected, scoped, and documented for each program according to the architecture, operating environment, technical risk, and agreed delivery requirements.

01

ELECTRICAL BRING-UP

Power-rail sequencing and ripple measured under load. Current draw profiled at idle, nominal, and peak actuation. Rails are checked against design margin before firmware bring-up.

02

BUS & TIMING VERIFICATION

SPI, I²C, UART, and CAN traffic captured on a logic analyzer. Clock integrity, setup/hold margins, and bus contention checked against each peripheral's datasheet timing.

03

SENSOR CHARACTERIZATION

IMU noise density, bias stability, and barometric drift recorded during characterization. Fusion output is compared against a reference where the program requires it.

04

HARDWARE-IN-THE-LOOP

Firmware exercised against simulated flight profiles: nominal, degraded-sensor, and fault-injection runs, as part of pre-delivery verification.

Verification scope is defined per program. Test records are shared with the customer as agreed in the program documentation.

Verification scope, acceptance criteria, test evidence, and technical records are defined within the program documentation and shared with the customer as agreed.

// SYS-NEXT · ENGAGE

BUILD SOMETHING LIKE THIS

Share a non-confidential overview of your platform, operating requirements, interfaces, and technical constraints. SWORT will review the requirement and respond with an appropriate next step, proposed scope, or request for a technical discussion.