Autonomous aerospace systems require architectures that balance deterministic real-time control with advanced perception capabilities. This paper presents an integrated system combining NASA's F' flight software framework with ROS2 middleware via Protocol Buffers bridging. We evaluate the architecture through a 32.25-minute indoor quadrotor flight test using vision-based navigation. The vision system achieved 87.19 Hz position estimation with 99.90% data continuity and 11.47 ms mean latency, validating real-time performance requirements. All 15 ground commands executed successfully with 100 % success rate, demonstrating robust F'--PX4 integration. System resource utilization remained low (15.19 % CPU, 1,244 MB RAM) with zero stale telemetry messages, confirming efficient operation on embedded platforms. Results validate the feasibility of hybrid flight-software architectures combining certification-grade determinism with flexible autonomy for autonomous aerial vehicles.
Figures & tables
Feature
F ′ [ 3 ]
cFS [ 8 ]
ROS 2 [ 7 ]
Domain
Flight
Flight avionics
Robotics
Execution
Deterministic
Modular services
Pub–sub
Memory
Static
Static
Dynamic
Fault mgmt
Yes
Yes
Ext./custom
QoS
Limited
Limited
DDS QoS
Certifiable
High
High
Low–Med
TABLE I: Comparison of autonomy and flight frameworks
Fig. 1: Software evolution: cFS → F ′→ ROS 2 → Space ROS.
Fig. 2: Hybrid architecture: F ′ for flight-critical logic; ROS 2 for perception/autonomy; bridge for telemetry/commands.
Bringing an aerial robotics method from simulation to flight should not require rebuilding a mature autopilot or adding a companion computer. Cybflight is an open-source embedded Rust research autopilot whose typed, replaceable interfaces connect hardware access, perception, state estimation, trajectory planning, and control. This modular development and compile-time optimization workflow is demonstrated with replaceable Rust implementations of model predictive contour-tracking control (MPCTC) and incremental nonlinear dynamic inversion (INDI) running on one STM32H743 without a companion computer. Using this configuration, the vehicle reaches 12.38 m/s during indoor flight, while an outdoor flight using global navigation satellite system (GNSS) position updates reaches 31.4 m/s. These flights show that running demanding estimation and nonlinear control entirely on a flight-controller microcontroller need not come at the expense of a modular autopilot structure.
Yifan Lin, Chao Qin, H S Helson Go +1
Institute for Aerospace Studies, University of Toronto, Toronto, Canada
ROScopter is a lean multirotor autopilot built for researchers. ROScopter seeks to accelerate simulation and hardware testing of research code with an architecture that is both easy to understand and simple to modify. ROScopter is designed to interface with ROSflight 2.0 and runs entirely on an onboard flight computer, leveraging the features of ROS 2 to improve modularity. This work describes the architecture of ROScopter and how it can be used to test application code in both simulated and hardware environments. Hardware results of the default ROScopter behavior are presented, showing that ROScopter achieves similar performance to another state-of-the-art autopilot for basic waypoint-following maneuvers, but with a significantly reduced and more modular code-base.
The integration of Vision-Language Models (VLMs) in autonomous Unmanned Aerial Vehicles (UAVs) offers unprecedented semantic reasoning capabilities. However, real-time closed-loop navigation requires not only low inference latency but also obedience to structured flight commands. This paper proposes a hybrid FSM-VLM control architecture for UAVs in GPS-free environments. The system combines a deterministic Finite State Machine (FSM) for low-level physical control with an asynchronous VLM copilot for high-level semantic pathfinding. We evaluate three models with different parameter scales in a Software-In-The-Loop (SITL) simulation. The framework isolates and measures syntax errors at the format level versus semantic hallucinations at the logic level in a normal and degraded scenario. This study demonstrates that parameter scaling, and not pure latency, remains the primary bottleneck for the safe and compatible integration of VLM into autonomous flights.
Hiago Sodre, Sebastian Barcelona, Vincent Sandin +6