A remote sensing system, comprising: - an air towable housing configured to carry one or more sensors configured to execute the measures of the remote sensing ; - an aircraft configured to tow the air towable housing ; - at least a first pulley , and - one or more attachment elements , each attachment element being a single string, rope, cable or wire which is wound around each of the at least one of said first pulley(s) thereby connecting the air towable housing to the aircraft such that each attachment element is attached in a suspension having at least three attachment places, wherein - a first attachment place is located on the housing , - a second attachment place is located on a first place of the aircraft , the remote sensing system being characterized in that : - a third attachment place is located on a second place of the aircraft , wherein the at least first pulley is attached to the first attachment place, or the at least first pulley is attached to the second attachment place and a second pulley is attached to the third attachment place; whereby the second attachment place and the third attachment place are spaced on the aircraft along a horizontal direction perpendicular to a motion direction of the aircraft when towing the housing and located on opposite sides of the aircraft with respect to said motion direction of the aircraft; whereby the suspension by the at least three attachment places connects the air towable housing to the aircraft , such that movement of the air towable housing relative to the aircraft along said horizontal direction enforces rotation of the at least one pulley , whereby the pulley or pulleys are mounted on bearings which are configured to produce internal friction when each pulley is rotated, said produced friction being configured to dampen the movement along said horizontal direction. - an air towable housing configured to carry one or more sensors configured to execute the measures of the remote sensing ; - an aircraft configured to tow the air towable housing ; - at least a first pulley , and - one or more attachment elements , each attachment element being a single string, rope, cable or wire which is wound around each of the at least one of said first pulley(s) thereby connecting the air towable housing to the aircraft such that each attachment element is attached in a suspension having at least three attachment places, wherein - a first attachment place is located on the housing , - a second attachment place is located on a first place of the aircraft , - a first attachment place is located on the housing , - a second attachment place is located on a first place of the aircraft , the remote sensing system being characterized in that : - a third attachment place is located on a second place of the aircraft , - a third attachment place is located on a second place of the aircraft , wherein the at least first pulley is attached to the first attachment place, or the at least first pulley is attached to the second attachment place and a second pulley is attached to the third attachment place; whereby the second attachment place and the third attachment place are spaced on the aircraft along a horizontal direction perpendicular to a motion direction of the aircraft when towing the housing and located on opposite sides of the aircraft with respect to said motion direction of the aircraft; whereby the suspension by the at least three attachment places connects the air towable housing to the aircraft , such that movement of the air towable housing relative to the aircraft along said horizontal direction enforces rotation of the at least one pulley , whereby the pulley or pulleys are mounted on bearings which are configured to produce internal friction when each pulley is rotated, said produced friction being configured to dampen the movement along said horizontal direction. <EOS>