초록 ▼

A highly reliable aerodynamic coefficient estimate can be computed, and computation of this aerodynamic coefficient estimate enables accurate detection of control surface failure/damage while reducing a discomfort for passengers. A deflection angle command signal generation means (5) generates a def

A highly reliable aerodynamic coefficient estimate can be computed, and computation of this aerodynamic coefficient estimate enables accurate detection of control surface failure/damage while reducing a discomfort for passengers. A deflection angle command signal generation means (5) generates a deflection angle command signal for estimating an aerodynamic coefficient indicating the aerodynamic characteristics of an airframe. A kinetic state quantity acquisition means (6) acquires a kinetic state quantity of the airframe that is obtained as a result of a control surface provided on the airframe being moved based on the deflection angle command signal. A candidate value calculation means (7) calculates candidate values for estimating the aerodynamic coefficient from the kinetic state quantity using two or more different estimations. An aerodynamic coefficient estimate determination means (8) determines an aerodynamic coefficient estimate based on the candidate values.

대표청구항 ▼

1. An aerodynamic coefficient estimation device comprising: a deflection angle command signal generation unit that generates a deflection angle command signal for estimating an aerodynamic coefficient indicating an aerodynamic characteristic of an airframe;a kinetic state quantity acquisition unit t

1. An aerodynamic coefficient estimation device comprising: a deflection angle command signal generation unit that generates a deflection angle command signal for estimating an aerodynamic coefficient indicating an aerodynamic characteristic of an airframe;a kinetic state quantity acquisition unit that acquires a kinetic state quantity of the airframe that is obtained as a result of a control surface provided on the airframe being moved based on the deflection angle command signal;a candidate value calculation unit that calculates candidate values for estimating the aerodynamic coefficient from the kinetic state quantity using two or more different estimations; andan aerodynamic coefficient estimate determination unit that determines an aerodynamic coefficient estimate based on the candidate values. 2. The aerodynamic coefficient estimation device according to claim 1, wherein the aerodynamic coefficient estimate determination unit determines an average or a median of the candidate values as an aerodynamic coefficient estimate. 3. The aerodynamic coefficient estimation device according to claim 1, wherein the aerodynamic coefficient estimate determination unit determines a candidate value corresponding to one of reproduced values of the kinetic state quantity that are computed respectively based on the candidate values as an aerodynamic coefficient estimate, the one reproduced value being the closest to the kinetic state quantity. 4. A control surface failure/damage detection device comprising: a failure/damage possibility judging unit that judges the possibility of control surface failure/damage;the aerodynamic coefficient estimation device according to claim 1; anda control surface failure/damage detection unit that detects which control surface suffers a failure or damage based on an aerodynamic coefficient estimate estimated by the aerodynamic coefficient estimation device if the failure/damage possibility judging unit judges that there is a possibility that control surface failure/damage may occur. 5. The control surface failure/damage detection device according to claim 4, wherein the failure/damage possibility judging unit includes:another deflection angle command generation unit that generates a deflection angle command signal for moving the control surface such that the airframe makes no motion; andanother kinetic state quantity acquisition unit that acquires a kinetic state quantity of the airframe that is obtained as a result of the control surface provided on the airframe being moved based on the deflection angle command signal, andthe possibility of control surface failure/damage is judged based on the kinetic state quantity. 6. The control surface failure/damage detection device according to claim 4, wherein the failure/damage possibility judging unit includes:still another deflection angle command signal generation unit that generates a deflection angle command signal for changing or maintaining the airframe to or in a desired attitude;still another kinetic state quantity acquisition unit that acquires a kinetic state quantity of the airframe during a flight based on the deflection angle command signal; anda kinetic state quantity prediction unit that computes a kinetic state quantity predictive value representing a kinetic state quantity that is predicted assuming that the airframe is in a normal state, andthe possibility of control surface failure/damage is judged based on the kinetic state quantity and the kinetic state quantity predictive value. 7. The control surface failure/damage detection device according to claim 4, comprising: an optical fiber or an electric wire laid on the airframe; anda detection unit that detects an abnormality of the optical fiber or the electric wire,wherein the failure/damage possibility judging unit includes:still another deflection angle command signal generation unit that generates a deflection angle command signal for changing or maintaining the airframe to or in a desired attitude;a deflection angle acquisition unit that acquires a deflection angle that is obtained as a result of the control surface provided on the airframe being moved based on the deflection angle command signal; anda deflection angle prediction unit that computes a deflection angle predictive value representing a deflection angle that is predicted based on the deflection angle command signal assuming that the airframe is in a normal state, andthe possibility of damage to the control surface is judged based on the detection result of the detection unit, and the possibility of a failure of the control surface is judged based on the deflection angle and the deflection angle predictive value. 8. The control surface failure/damage detection device according to claim 4, wherein the control surface failure/damage detection unit detects a failure of or damage to the control surface by comparing the aerodynamic coefficient estimate with either an aerodynamic coefficient estimate of the airframe in a normal state or an aerodynamic coefficient estimate that was obtained when failure/damage detection was performed the previous time.