A system (100/300) for determining drift of an aircraft from hover, comprising: one or more sensors configured to detect velocity of the aircraft and/or a position of the aircraft at different time intervals; a combined modality drift cueing controller coupled to the one or more sensors, the combined modality drift cueing controller being configured to determine drift of the aircraft from hover and configured to control a plurality of indicators in response to determined drift; and a mode selector coupled to the combined modality drift cueing controller and configured to provide an indication of mode selection between one of a first mode, a second mode and a third mode; the system (100/300) being characterized in that it further comprises: a peripheral vision drift indicator (106/108/110/302/304/306/308) coupled to the combined modality drift cueing controller and mountable on an inside surface of a cockpit of an aircraft, the peripheral vision drift indicator including a first drift indicator (106/302/304) configured to indicate fore/aft drift and mountable on a door frame of the aircraft adjacent to a pilot seat so as to be visible in a peripheral vision field of an individual seated in the pilot seat; and a tactile feedback indicator coupled to the combined modality drift cueing controller, wherein a drift cueing signal is sent to both the peripheral vision drift indicator and the tactile feedback indicator when the mode selector is in the first mode, wherein the drift cueing signal is sent to only the peripheral vision drift indicator when the mode selector is in the second mode and wherein the drift cueing signal is sent to only the tactile feedback indicator when the mode selector is in the third mode. one or more sensors configured to detect velocity of the aircraft and/or a position of the aircraft at different time intervals; a combined modality drift cueing controller coupled to the one or more sensors, the combined modality drift cueing controller being configured to determine drift of the aircraft from hover and configured to control a plurality of indicators in response to determined drift; and a mode selector coupled to the combined modality drift cueing controller and configured to provide an indication of mode selection between one of a first mode, a second mode and a third mode; the system (100/300) being characterized in that it further comprises: a peripheral vision drift indicator (106/108/110/302/304/306/308) coupled to the combined modality drift cueing controller and mountable on an inside surface of a cockpit of an aircraft, the peripheral vision drift indicator including a first drift indicator (106/302/304) configured to indicate fore/aft drift and mountable on a door frame of the aircraft adjacent to a pilot seat so as to be visible in a peripheral vision field of an individual seated in the pilot seat; and a tactile feedback indicator coupled to the combined modality drift cueing controller, wherein a drift cueing signal is sent to both the peripheral vision drift indicator and the tactile feedback indicator when the mode selector is in the first mode, wherein the drift cueing signal is sent to only the peripheral vision drift indicator when the mode selector is in the second mode and wherein the drift cueing signal is sent to only the tactile feedback indicator when the mode selector is in the third mode.