Verification framework for control theory of aircraft

Abstract A control system verification framework is presented for unmanned aerial vehicles using theorem proving. The framework’s aim to set out a procedure proving that the mathematically designed of aircraft satisfies robustness requirements ensure safe performance under varying environmental conditions. Extensive mathematical derivations, which have formerly been carried manually, are checked their correctness on computer. To illustrate procedures, higher-order logic interactive theorem-prover and an automated utilised formally verify nonlinear attitude generic multi-rotor UAV over stability domain within dynamical state space drone. Further benefits procedures some resulting methods can be implemented onboard detect when its controller breaches flight envelope limits due severe weather conditions or actuator/sensor malfunction. Such detection used advise remote pilot, intelligent agent, decide alterations planned path perform emergency landing.