Miguel Angel Silva Plata

Mr. Miguel Angel Silva Plata

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Research Focus & Metrics

Academic Career Length

3Years (2024-Present)

(Calculated once Scilit publication data is synced: current year − year of first publication + 1)

Representative Publications

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11 July 2024 in Applied Sciences
Verified
Journal Article
Open access
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Franklin Josue Ticona CoaquiraFranklin Josue Ticona Coaquira
Franklin Josue Ticona Coaquira
Xinsheng WangXinsheng Wang
Xinsheng Wang
KTKaren Wendy Vidaurre Torrez
Karen Wendy Vidaurre Torrez
MQMisael Jhamel Mamani Quiroga
Misael Jhamel Mamani Quiroga
MPMiguel Angel Silva Plata
Miguel Angel Silva Plata
ARArturo Rojas
Arturo Rojas
This study introduces a robust model-based framework designed for the verification and validation (V&V) of Attitude Determination and Control Systems (ADCSs) in nanosatellites, focusing on magnetic actuation while still being applicable to larger spacecraft platforms. By employing Model-in-the-Loop (MIL), Software-in-the-Loop (SIL), Processor-in-the-Loop (PIL), and Hardware-in-the-Loop (HIL) methodologies, this framework enables a thorough and systematic approach to testing and validation. The framework facilitates the assessment of long-term maneuvers, addressing challenges such as initial small-attitude errors and restricted 3D movements. Two specific maneuvers are evaluated: detumbling and nadir pointing, utilizing quaternions and a comprehensive suite of sensors, including six sun sensors, a three-axis magnetometer, a three-axis gyroscope, GPS, and three magnetorquers. The methodologies—MIL, SIL, PIL, and HIL—integrate the behaviors of digital sensors, analog signals, and astrodynamic perturbations. Based on an optimized SIL environment, Monte Carlo simulations were performed to optimize control gains for nadir pointing, achieving a mean pointing accuracy of 11.69° (MIL) and 18.22° (PIL), and an angular velocity norm of 0.0022 rad/s for detumbling. The HIL environment demonstrated a mean pointing accuracy of 9.96° and an angular velocity norm of 0.0024 rad/s. This comprehensive framework significantly advances the design and verification processes for nanosatellite ADCSs, enhancing the reliability and performance of nanosatellite missions.

29 May 2026 in IEEE Robotics & Automation Magazine
Verified
Journal Article
Closed access
CSCarolina Silva-plata
Carolina Silva-plata
AVAbraham Villavicencio-Carmona
Abraham Villavicencio-Carmona
MPMiguel Angel Silva Plata
Miguel Angel Silva Plata
SEStefan Escaida
Stefan Escaida
RURuben Marcos Fernandez Urrutia
Ruben Marcos Fernandez Urrutia
Soft robotics is increasingly explored in artistic contexts, where tactile interaction provides audiences with embodied engagement beyond visual or auditory signals. This article presents an interactive installation that maps semantic emotion analysis of narrative text into variable stiffness of soft pneumatic modules. A natural language model identifies two dominant emotions from a predefined set of six, driving the inflation of seven hexagonally arranged soft actuators. The central actuator represents the primary emotion, while the surrounding ones express the secondary one. We develop and mechanically characterize silicone actuators, called soft modules, featuring a thin membrane layer, demonstrating how this morphological control expands the achievable stiffness range while preserving simplicity and low-cost fabrication. A user study with 10 participants further evaluates how multisensory coupling of stiffness and LED intensity influences emotional perception. The results suggest that stiffness modulation accompanied by color change can support emotionally meaningful and engaging tactile interaction in soft robotic installations.