Event-Triggered Intermittent Prescribed Performance Control for Spacecraft Attitude Reorientation
Jiakun Lei, Tao Meng, Kun Wang, Weijia Wang, Zhonghe Jin

TL;DR
This paper introduces an event-triggered intermittent control scheme for spacecraft attitude reorientation that reduces actuator frequency while ensuring prescribed performance, combining a composite event-trigger mechanism with PPC and validated through simulations.
Contribution
It proposes a novel composite event-trigger mechanism integrated with prescribed performance control for spacecraft, addressing the gap between continuous control design and discrete implementation.
Findings
Significantly reduces actuator actuation frequency.
Maintains desired attitude control performance.
Validated effectiveness through numerical simulations.
Abstract
This paper focuses on the issue of how to realize spacecraft attitude control with guaranteed performance while conspicuously reducing the actuator acting frequency simultaneously. The prescribed performance control (PPC) scheme is often employed for the control with guaranteed performance. However, conventional PPC controllers are designed from the perspective of continuous system, which contradicts the "discrete" control logic in actual spacecraft control system, and such a problem limited the application value of PPC scheme in actual applications. In order to significantly lower the actuator acting frequency while still maintaining the desired performance, a composite event-trigger mechanism is proposed for this issue, turning off the actuator and eliminating unnecessary control output under appropriate conditions. Further, the proposed composite event-trigger mechanism is combined…
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Taxonomy
TopicsAdaptive Control of Nonlinear Systems · Stability and Control of Uncertain Systems · Inertial Sensor and Navigation
