Morph
Engine 02 / 05 · Design & Code · Independent
Design and code written for proof —
every line carries a contract a verifier can discharge.
Explore more ↓FROM ARCHITECTURE TO OBJECT CODE
System design through to flight-grade software
System design & architecture
Decomposes a concept into subsystems, interfaces, and budgets — with the rationale recorded.
Control-law implementation
From validated math to deterministic real-time code, with timing and numeric range analysis.
Flight code — Ada/SPARK & C/C++
Contract-rich, statically provable code; MISRA-conformant C/C++ where the target demands it.
Model-based design — MATLAB/Simulink
Models, autocode review, and back-to-back testing between model and target.
Assembly & low-level routines
Startup, interrupt, and driver code for the boards avionics shops actually fly.
Static verification & proof
Proof obligations discharged and reported — no runtime errors, ranges respected.
A WORKED ARTIFACT
Software that proves its properties
MORPH delivers the design rationale, the governing requirement, the implementation, and the discharged proof obligations — evidence a reviewer can replay rather than take on faith.
REQ REQ-FCS-031 · limit commanded pitch rate to ±12 °/s
TARGET Ada/SPARK · DAL B · deterministic, no heap
DESIGN saturating limiter ahead of the actuator command path
-- SPARK: contract carries the requirement
procedure Limit_Pitch_Rate (Cmd : in out Deg_Per_S)
with Post => abs Cmd <= Max_Pitch_Rate
and Max_Pitch_Rate = 12.0;PROVE GNATprove · 14 / 14 checks proved · no runtime errors
VERIFIED · TRACEABLE TO FIRST PRINCIPLES
THE REMAINING ENGINES
Independent peers
None depends on this engine's output. Open the one your current task calls for.
MORPH · AEROSPACE INTELLIGENCE