Reliability-Aware Supervisory Flight Control of Quadrotors Using Causal Condition Estimation
Abstract Quadrotor flight control under time-varying uncertainty is challenging because no single controller remains uniformly superior across nominal operation, payload variation, wind disturbance, and rotor degradation. This study presents a reliability-aware supervisory flight-control architecture that selects between adaptive proportional–integral–derivative control and linear quadratic regulation using causal condition estimation and requirement-conditioned reliability information. The framework combines controller-conditioned estimation of payload, wind magnitude, rotor effectiveness, and affected-rotor identity with reliability-based decision logic, asymmetric fault latching, hysteresis, dwell time, decision persistence, and bumpless command transfer. The estimator operates causally using a 0.50 s trailing window updated every 0.25 s. Once rotor degradation is confirmed, the fault state is permanently latched and post-fault reversal from linear quadratic regulation to adaptive PID is prohibited. The final architecture was evaluated exclusively in nonlinear simulation using 500 independent stratified missions comprising payload/wind-dominant, rotor-degradation-dominant, sequential mixed, and boundary scenarios, resulting in 2,000 paired simulations. The practical supervisor achieved 71.2% mission reliability, compared with 35.0% for fixed adaptive PID and 25.4% for fixed LQR, while matching the perfect-information oracle in all 500 missions. The improvement over both fixed controllers was statistically significant, and the practical architecture satisfied a predeclared 5 percentage-point noninferiority margin relative to the oracle. Successful-mission median tracking error increased by only 1.65% relative to the oracle. The estimator achieved 91.31% rotor-fault recall, a 0.326% false-positive rate, 0.393 s median causal detection delay, and 100% rotor-identity accuracy. These results demonstrate that causal condition estimation and asymmetric reliability-aware supervision can recover oracle-level mission reliability without requiring perfect operating-condition knowledge within the modeled operating envelope.
Authors
- Julian Bardin
- Mohsen Rostami (ORCID: https://orcid.org/0000-0003-1296-9751)
- Joon Chung (ORCID: https://orcid.org/0000-0001-8679-9308)
- Alessandro Ciniello
Institutions
- Toronto Metropolitan University (CA)
Publication Details
- Journal
- Research Square
- Published
- 2026-11-11
- DOI
- https://doi.org/10.21203/rs.3.rs-11423089/v1
- Primary Topic
- Adaptive Control of Nonlinear Systems
- Type
- preprint