Abstract: A method for controlling an aircraft when taxiing comprising the steps of: measuring an angle of rotation of an active side stick about a first axis and a second axis; receiving an aircraft signal representative of an actual state of the aircraft; generating a control signal based on at least one of: the aircraft signal and the angle of rotation of the active side stick about a first axis and a second axis; transmitting the control signal to the aircraft, whereby the control signal causes an action affecting the actual state of the aircraft; determining a required state of the aircraft; generating a user feedback signal based on at least one difference between the actual state and the required state; and carrying out a user feedback action based on the user feedback signal.

Abstract: A biscuit or cookie and method of manufacture of same includes forming a quantity of unbaked dough into a shaped, unbaked dough piece. A network of lines comprising grooves is impressed into the upper surface of the unbaked dough piece, either in conjunction with or subsequent to forming of the dough piece. A major portion of the lines in the network are non-terminated lines which continue across the surface of the dough piece and intersect either the edge of the dough piece or another line, and a minor portion of the lines are terminated lines which end short of either the edge or another line at least at one end thereof. The shaped dough piece with the network of impressed lines is baked under such conditions as to increase its diameter by from one-tenth to one-half and to form superficial fissures along at least some of the impressed lines and at least in some of the areas of the upper surface of the dough piece upon which lines were not previously impressed.