A flight control computer for a rotorcraft, comprising: a processor; and a non-transitory computer-readable storage medium storing a program to be executed by the processor, the program including instructions for: receiving one or more signals indicating a weight on wheels count associated with a number wheels of the rotorcraft that bear weight of the rotorcraft; providing a first set of integrators in a first set of hold loops that generate first control augmentation signals for a flight system of the rotorcraft; providing a second set of integrators in a second set of hold loops that generate second control augmentation signals for the flight system; maintaining a WOW state machine having at least a single gear state and an in transit state; determining an active WOW state of the WOW state machine according to at least the WOW count; freezing the first set of integrators in response to determining that the single gear state is the active WOW state, wherein the first set of hold loops generate the first control augmentation signals according to first values provided by the first set of integrators when the first set of integrators are frozen; and freezing the second set of integrators in response to determining that the in transit state is the active WOW state, wherein the second set of hold loops generate the second control augmentation signals according to second values provided by the second set of integrators when the second set of integrators are frozen; wherein the first set of hold loops includes at least a position hold loop, a speed hold loop, and a heading hold loop, and wherein the second set of hold loops includes at least the position hold loop, the speed hold loop, the heading hold loop, and an attitude hold loop. a processor; and a non-transitory computer-readable storage medium storing a program to be executed by the processor, the program including instructions for: receiving one or more signals indicating a weight on wheels count associated with a number wheels of the rotorcraft that bear weight of the rotorcraft; providing a first set of integrators in a first set of hold loops that generate first control augmentation signals for a flight system of the rotorcraft; providing a second set of integrators in a second set of hold loops that generate second control augmentation signals for the flight system; maintaining a WOW state machine having at least a single gear state and an in transit state; determining an active WOW state of the WOW state machine according to at least the WOW count; freezing the first set of integrators in response to determining that the single gear state is the active WOW state, wherein the first set of hold loops generate the first control augmentation signals according to first values provided by the first set of integrators when the first set of integrators are frozen; and freezing the second set of integrators in response to determining that the in transit state is the active WOW state, wherein the second set of hold loops generate the second control augmentation signals according to second values provided by the second set of integrators when the second set of integrators are frozen; wherein the first set of hold loops includes at least a position hold loop, a speed hold loop, and a heading hold loop, and wherein the second set of hold loops includes at least the position hold loop, the speed hold loop, the heading hold loop, and an attitude hold loop. receiving one or more signals indicating a weight on wheels count associated with a number wheels of the rotorcraft that bear weight of the rotorcraft; providing a first set of integrators in a first set of hold loops that generate first control augmentation signals for a flight system of the rotorcraft; providing a second set of integrators in a second set of hold loops that generate second control augmentation signals for the flight system; maintaining a WOW state machine having at least a single gear state and an in transit state; determining an active WOW state of the WOW state machine according to at least the WOW count; freezing the first set of integrators in response to determining that the single gear state is the active WOW state, wherein the first set of hold loops generate the first control augmentation signals according to first values provided by the first set of integrators when the first set of integrators are frozen; and freezing the second set of integrators in response to determining that the in transit state is the active WOW state, wherein the second set of hold loops generate the second control augmentation signals according to second values provided by the second set of integrators when the second set of integrators are frozen; wherein the first set of hold loops includes at least a position hold loop, a speed hold loop, and a heading hold loop, and wherein the second set of hold loops includes at least the position hold loop, the speed hold loop, the heading hold loop, and an attitude hold loop.