
Contributed to the Space-and-Satellite-Systems-UC-Davis/ADCS-Software repository by developing and integrating a PID-based angular velocity control system for attitude determination and control. Leveraging C programming and embedded systems expertise, implemented in-loop PID experimentation and dual hard-disk drive (HDD) output, establishing a foundation for automated tuning and safer, more responsive control. Enhanced the ADCS main loop with new interfaces and refined termination logic, while introducing execution rate regulation for improved precision. The work included code refactoring and cleanup of HDD arming and logging, supporting robust testing and future experimental validation. Focus remained on maintainability, real-time control, and firmware development.
May 2025: ADCS software development focused on delivering a robust PID-based angular velocity control, with multi-HDD output, accompanied by incremental HDD arming/logging cleanup and refactors to enable testing. The work establishes a foundation for repeatable experiments and safer attitude control with higher responsiveness.
May 2025: ADCS software development focused on delivering a robust PID-based angular velocity control, with multi-HDD output, accompanied by incremental HDD arming/logging cleanup and refactors to enable testing. The work establishes a foundation for repeatable experiments and safer attitude control with higher responsiveness.
April 2025: Delivered integration of PID Experiment into the ADCS software, establishing in-loop experimentation capability and groundwork for automated PID tuning. Implemented new interfaces in virtual_intellisat.h and new PID_experiment.c implementations to initiate and arm the HDD for the PID run, enabling execution within the ADCS main loop. Tightened the PID termination condition and added a rate-regulating delay to stabilize execution for more precise control. These changes provide a solid testbed for PID tuning, faster validation cycles, and reduced risk in flight software development.
April 2025: Delivered integration of PID Experiment into the ADCS software, establishing in-loop experimentation capability and groundwork for automated PID tuning. Implemented new interfaces in virtual_intellisat.h and new PID_experiment.c implementations to initiate and arm the HDD for the PID run, enabling execution within the ADCS main loop. Tightened the PID termination condition and added a rate-regulating delay to stabilize execution for more precise control. These changes provide a solid testbed for PID tuning, faster validation cycles, and reduced risk in flight software development.

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