
Developed a Roll Control System (RCS) for the Avionics-Propulsion-Landers-GT/MonopropUAV repository, focusing on enhancing roll stability and maneuverability in rocket and UAV simulations. The solution applied control theory by designing LQR-based gains, validated through MATLAB-based dynamics and control simulations. Implementation involved creating a modular RcsController struct in Rust, encapsulating control parameters and logic for reuse across flight scenarios. The RCS was integrated into the simulation pipeline by updating algorithms.rs, enabling end-to-end roll control within the existing framework. Work emphasized robust algorithm development, software integration, and codebase stabilization, with traceable commits and no major bugs reported during the period.
April 2026 monthly summary — Avionics-Propulsion-Landers-GT/MonopropUAV: - Delivered Roll Control System (RCS) with LQR gains to improve stability and maneuverability in roll dynamics for rocket/UAV simulations. The system includes LQR-based tuning, MATLAB-based dynamics and control simulations, and a Rust-based command structure for thruster firing. The RcsController struct encapsulates control parameters and logic for reuse across flight scenarios. - Integrated the RCS into the simulation pipeline by updating algorithms.rs, enabling end-to-end roll control within the existing flight dynamics framework. - Established traceability with two commits (a70ff99fa843a814ea12af0061278e229f03e76d; 9bccb6c1198b6ab7b50872bbc3d5d5a77377797a). - Overall impact: enhanced fidelity of roll dynamics, improved stability and maneuverability, and a reusable control module for future propulsion tests and mission scenarios. - Technologies/skills demonstrated: control theory (LQR), MATLAB simulations, Rust-based system design, modular Rust struct (RcsController), software integration (algorithms.rs).
April 2026 monthly summary — Avionics-Propulsion-Landers-GT/MonopropUAV: - Delivered Roll Control System (RCS) with LQR gains to improve stability and maneuverability in roll dynamics for rocket/UAV simulations. The system includes LQR-based tuning, MATLAB-based dynamics and control simulations, and a Rust-based command structure for thruster firing. The RcsController struct encapsulates control parameters and logic for reuse across flight scenarios. - Integrated the RCS into the simulation pipeline by updating algorithms.rs, enabling end-to-end roll control within the existing flight dynamics framework. - Established traceability with two commits (a70ff99fa843a814ea12af0061278e229f03e76d; 9bccb6c1198b6ab7b50872bbc3d5d5a77377797a). - Overall impact: enhanced fidelity of roll dynamics, improved stability and maneuverability, and a reusable control module for future propulsion tests and mission scenarios. - Technologies/skills demonstrated: control theory (LQR), MATLAB simulations, Rust-based system design, modular Rust struct (RcsController), software integration (algorithms.rs).

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