Methods and apparatus to control camber

A tangible machine readable medium comprising instructions, which when executed, cause a processor to at least:

• determine that a flap of an aircraft has been rotated, via a flap support actuator, relative to a neutral position associated with an aerodynamic surface, wherein the flap support actuator moves a drive arm linkage that is rotatably coupled to a flap support at a first pivot of the flap support, and wherein the drive arm linkage includes a second pivot at an end opposite the first pivot;
• determine a flight parameter of the aircraft during a cruise flight stage of the aircraft;
• calculate an adjustment flap angle based on the flight parameter;
• and
• control movement of a camber control actuator based on the adjustment flap angle to adjust an angle of the flap, wherein the camber control actuator is rotatably coupled to a third pivot of the flap support and a fourth pivot associated with the flap.