Investment
Access approved company materials, product milestones, traction, and the roadmap for SSIL and protected advanced programs.
Investor Access →SWORT · Aerospace Electronics Systems & Defense Avionics Hardware | US-Based Engineering
AEROSPACE ELECTRONICS SYSTEMS
// SYS-RTE-00 · DIRECT YOUR INQUIRY
01 / I Represent
A DEFENSE OR AEROSPACE PROGRAM
Program-scale avionics under NDA. Requirements-driven scoping, export-control-aware handling, and full documentation packages.
Submit requirements → 02 / I Represent A RESEARCH OR UNIVERSITY TEAMFlight computers, telemetry, and recovery electronics for competition and research vehicles, delivered flight-ready with source.
Submit requirements → 03 / I'd Rather TALK TO AN ENGINEER FIRSTA 45-minute technical brief with the engineering team. Scope, feasibility, and timeline, before any commitment.
Book a session →// Operating foundation
SAM.gov
Active Registration
CAGE
21UQ1
Primary NAICS
541330 · Engineering Services
Entity
SWORT LLC · DBA SWORT Aerospace
Registration information does not imply government endorsement, contract award, certification, product qualification, or security clearance.
View Government Capabilities →// SYS-CAP-01
CAPABILITIES
Mission-critical avionics systems and embedded aerospace hardware, engineered to specification, delivered with full documentation.
01
FLIGHT COMPUTER SYSTEMS
STM32H7-based embedded flight computers engineered to mission parameters. Deterministic real-time processing, multi-sensor integration, SD telemetry logging. Delivered with full firmware source, schematic, and BOM.
02
GNC HARDWARE
Guidance, navigation, and control hardware purpose-built to vehicle requirements. IMU, GPS, and barometer sensor fusion with EKF/UKF attitude estimation. Configurable actuator output interfaces for closed-loop flight control.
03
CUSTOM PCB DESIGN
Aerospace PCB design with schematic capture and layout in KiCad or Altium. DFM-reviewed Gerbers, full BOM, and assembly drawings. Manufactured and bench-tested boards delivered integration-ready.
04
TELEMETRY SYSTEMS
LoRa-based telemetry systems with real-time ground station dashboards. Configurable RF frequency, data rate, and packet format. Includes receiver hardware and ground-side software for any vehicle class.
05
RECOVERY ELECTRONICS
Redundant ejection charge controllers, dual-deploy sequencing, and continuity verification hardware. Designed to TRA and NAR safety standards. Bench-tested and verified against deployment parameters before delivery.
06
EMBEDDED FIRMWARE
Production-grade embedded firmware for STM32 and bare-metal RTOS platforms. Version-controlled, fully documented. Delivered with unit test suite and integration guide. Source-complete, no black boxes.
// SYS-PROC-02 · Engineering execution
FROM SYSTEM REQUIREMENTS
TO VALIDATED HARDWARE.
Five stages. Each one produces something reviewable before the next begins.
01
REQUIREMENTS & SYSTEM BOUNDARIES
Mission profile, vehicle, interfaces, environment, and hard constraints are captured first. What the system is responsible for, and what it is not, is written down before anything is designed.
02
ARCHITECTURE & INTERFACE DEFINITION
Subsystems, signal paths, buses, power budget, and sensor interfaces are defined. Register maps, timing, and the hardware-software boundary are agreed before layout or firmware starts.
03
HARDWARE & EMBEDDED IMPLEMENTATION
Schematic capture, layout, and DFM review on the hardware side. Firmware built against the defined interfaces on the software side. Boards are brought up from power rails through sensor validation.
04
INTEGRATION & FAULT INJECTION
Subsystems are integrated and then deliberately disagreed with. Sensor inconsistency, degraded channels, and induced faults are injected so the response is observed rather than assumed.
05
VERIFICATION & TECHNICAL HANDOFF
Results are checked against the acceptance criteria written in stage one. You receive the hardware with firmware source, schematics, BOM, wiring diagrams, and the test records behind the result.
// SYS-STD-03
ENGINEERING STANDARDS
Every system leaves the lab tested, traceable, and documented. This is how.
01
VERIFICATION & VALIDATION
Requirements are captured before design starts and verified before delivery. Firmware is exercised against unit tests and hardware-in-the-loop runs; boards are bench-tested against the acceptance criteria in your scope document.
02
REVISION CONTROL
All firmware, schematics, and layout files live in version control from day one. Every delivered artifact is tagged to a specific revision: you can trace any board or binary back to its exact source state.
03
QUALITY ASSURANCE
Static analysis and MISRA-informed coding standards on firmware. DFM review on every layout before fabrication. Continuity, power-rail, and functional checks on every assembled board before it ships.
04
DOCUMENTATION
Source-complete delivery: firmware source, schematics, BOM, wiring diagrams, and an integration guide in every package. No black boxes, no locked toolchains, no undocumented interfaces.
Engineering Practices & Objectives
Requirements-driven development
Practice
Revision-controlled engineering files
Practice
Designed with traceability in mind
Practice
Verification planning per program
Practice
ITAR-conscious project screening
Practice
Authorized-distributor sourcing where required
Practice
Traceable engineering execution: requirements, design records, revisions, and verification evidence under controlled workflow
Practice
These describe SWORT's internal engineering practices and forward objectives. They are not certifications, formal approvals, or third-party qualifications. Program-specific standards are agreed contractually.
// SYS-TECH-05 · SSIL
Cross-sensor state validation for autonomous platforms.
SSIL ingests synchronized navigation, inertial, magnetic, power, and environmental telemetry, evaluates residual consistency across sensor channels, and outputs source-level health, trust, and fault-state signals to the vehicle stack.
It operates as an independent integrity layer and does not replace the flight controller, estimator, or control law.
Public commercial architecture. Under active development.
SSIL
SYSTEM STATE INTEGRITY LAYER
Inputs
Navigation, inertial, magnetic, power, environmental
Evaluation
Residual consistency across sensor channels
Outputs
Source health, trust, fault state
Scope
Independent of flight control and estimation
INTERACTIVE DEMONSTRATION
Parameter-driven state model. Adjust sensor quality and disturbance and observe the resulting trust and fault-state response.
System Modules
Vehicle State
YAW 0.0°
PITCH 0.0°
ROLL 0.0°
MODE NOMINAL
Live Telemetry
Stability Score
--/ 100
Drift Vector
X
--
Y
--
Z
--
System Load
--%
Control Efficiency
--%
Technical description
SSIL compares each sensor channel against the others and against the state implied by vehicle motion. A channel that disagrees with the rest of the system has its contribution reduced rather than weighted equally, and the disagreement is reported as a probable source instead of a single pass or fail flag.
In the demonstration, raising sensor noise or environmental disturbance reduces cross-channel consistency, so the stability score falls, drift grows, and the mode indicator moves from nominal to degraded to critical. Raising control gain and sensor quality reverses it. Every value on the diagram is also listed as text in the Live Telemetry panel, so the behaviour can be followed without operating the controls.
// SYS-ENG-04
ENGAGEMENT
Engineering programs are scoped according to platform requirements, integration complexity, verification needs, and delivery scope.
01 / Requirements
We start from your platform, mission profile, interfaces, and constraints, not from a fixed package.
02 / Scope
Integration complexity and verification needs determine the work breakdown and the delivery schedule.
03 / Proposal
You receive a written scope, interface assumptions, and a delivery plan before any commitment.
// SYS-INTK-08
START A PROJECT
Submit a technical inquiry. We'll evaluate requirements scope and respond within 48 hours.
Prefer to talk first? Book a 45-minute session.
// Inside the work
Engineering happens at the bench.
SWORT develops and evaluates aerospace electronics through hardware review, embedded implementation, simulation, integration, and bench-level verification.
Development environments used by SWORT. Some development and verification takes place in shared technical facilities rather than premises owned by SWORT, and these images are not a claim of facility ownership.
// SYS-CAP-11 · Capital & R&D Partnerships
Support the next generation of aerospace sensor integrity.
SWORT works with qualified investors, technical sponsors, research institutions, and aerospace organizations pursuing advanced avionics and autonomous-system reliability.
R&D Partnerships
Sponsor a SWORT research program, propose a technical collaboration, or apply for support on aligned aerospace-electronics work.
Explore R&D Partnerships →Professional Affiliations
SWORT participates in professional engineering and aerospace communities that support continued technical development, standards awareness, and industry collaboration. Participation is a membership relationship, nothing more.
SWORT participates in the following professional bodies: AIAA (American Institute of Aeronautics and Astronautics), IEEE (Institute of Electrical and Electronics Engineers), ASME (American Society of Mechanical Engineers).
Organization names and marks remain the property of their respective owners. Membership or professional affiliation does not imply certification, sponsorship, endorsement, accreditation, or approval of SWORT Aerospace.
SWORT Network
Stay close to the work.
Engineering updates, research releases, open programs, and selected opportunities from SWORT Aerospace.
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// SYS-CREW-10
WORK WITH SWORT
Engineering-led. Hardware-focused. We build systems that meet defined requirements, not mock-ups, not simulations.
01
AVIONICS ENGINEERING
STM32 firmware, sensor integration, embedded C. You own subsystems end-to-end, from register-level bring-up to flight-ready delivery. Datasheets are your primary documentation.
View Role & Apply →02
GNC SOFTWARE DEVELOPER
Attitude estimation, Kalman filtering, and control loop implementation. Python or MATLAB for analysis, C for embedded targets. Experience with real sensor data preferred over simulation-only background.
View Role & Apply →03
PCB DESIGN CONTRIBUTOR
Schematic capture and layout in KiCad or Altium. DFM-aware design, proper impedance control, and clean Gerber output. You've taped out at least one board that actually worked.
View Role & Apply →