as shown in fig1 - 5 , the preferred embodiment of the mount comprises a gimbal unit assembly 51 having a vertical post assembly 55 , a central gimbal frame 15 , and gimbal end suspension assemblies 8 . the vertical gimbal post assembly 55 and the end suspension assemblies 8 are connected to the central gimbal frame 15 in a manner described more specifically below that permits a camera mounted to the vertical post assembly 55 to be moved freely and simultaneously through the yaw , roll , and pitch axes . the gimbal unit assembly 51 is suspended from elastic straps 7 that connect the end suspension assemblies 8 to hooks 11 on post blocks 1 which in turn are connected to a pair of posts 2 . this means of suspension dampens the vibrations of the aircraft that would otherwise be transmitted to the gimbal unit assembly 51 . as shown in fig1 and 3 , the vertical gimbal post assembly 55 comprises a camera mount base 16 for the attachment of a base mount plate 6 and tripod head 5 at the upper end and a gyro mount plate 10 for mounting gyroscopic stabilizers 13 at the bottom end . as shown in more detail in fig3 , a circular camera mount base 6 is fastened above the top post member 31 by a pair of screws 38 . an alternative , as depicted in fig1 and 5 , is to use a camera mount base 6 of the quick release variety . the bottom end of the top post member 31 is press fit to the inside the inner race of bearing 30 . the bearing 30 concurrently resides in a recess in the upper end of the middle post member 9 with a light push fit . a bronze bushing 33 is located beneath the bearing 30 but does not engage the bearing . the vertical gimbal post assembly 55 also comprises a bottom post member 32 in which the upper end is press fit to the inside of the inner race of bearing 28 . the bearing 28 concurrently resides in a recess at the lower end of the middle post member 9 with a light push fit . another bronze bushing 29 is located above the bearing 28 but does not engage the bearing . the top post member 31 is connected to the bottom post member 32 by a bolt 25 that extends though the center of the top post member 31 and through the middle post member 9 into the bottom post member where it engages a threaded section 61 and is further secured by a set screw 26 . this arrangement allows the top post member 31 and the bottom post member 32 to rotate freely relative to the middle post member 9 . as shown in fig1 , 2 , and 3 , a gyro mounting plate 10 is fastened to the bottom post member 32 by screws 27 . the gyro mounting plate 10 is preferably configured in a cruciform arrangement that enable gyroscopic stabilizers 13 to be mounted with their spin axes aligned respectively in parallel with the roll and yaw axes of the gimbal unit . if desired , an auxiliary gyroscopic stabilizer plate 23 may be fastened to the bottom end of the gyroscopic stabilizer plate 10 to enable a third gyroscopic stabilizer ( not shown ) to be mounted with its spin axis in parallel alignment with the pitch axis . similar , if desired , counterweights may be fastened to the gyroscopic stabilizer plate 10 or the auxiliary gyroscopic stabilizer plate 23 to provide ballast to ensure that the camera is maintained in a balanced position above the central gimbal frame 15 . also shown in fig3 , hollow spacers 36 have a proximal end that engage recesses on opposing sides of the middle post member 9 with a slight push fit . bushings 37 engages the inner side of the inner race of bearings 35 with a slight push fit . the bearings 35 are press fitted into recesses in opposing sides of the central gimbal frame 15 the bushings 37 are aligned with the spacers 36 and bolts 34 pass through the bushings 37 and the spacers 36 and secured to the threaded side openings 62 in the middle post member 9 so as to connect the vertical gimbal post assembly 55 to the central gimbal frame 15 . this arrangement allows the vertical post assembly 55 to pivot about the pitch axis . as shown in fig2 and 4 , the central gimbal frame 15 is connected to the gimbal end suspension assemblies 8 by side posts 21 . the side posts 21 consist of a cylindrical member with a threaded opening 38 a at the proximal end and a threaded opening 44 a at the distal end , the proximal end of the side post 21 is connected to the central gimbal frame 15 by a bolt 38 that is threaded into opening 38 a . the end suspension assembly 8 comprises a housing 45 to which a strap support post 24 is secured by screws 46 that pass through opposing sides of the housing 45 and are threaded into the strap support post 24 . the outer circumference of bearing 42 is press fit into the housing 45 . the small circumference ends of two shouldered bushings 43 and 43 a are press fit from opposite ends into the inner circumference of the bearing 42 . the large circumference end of bushing 43 a extends from the face of housing 45 and fits within a recess 39 of side post 21 such that a small gap 41 is present between the housing 45 and side post 21 . a bolt 44 passes through the hole in the bushing 43 and is threaded into opening 44 a thus securing the end suspension assembly 8 onto the side post 21 . this arrangement allows the central frame 15 to pivot about the roll axis when the mount is facing out from the side of an aircraft . as shown in fig1 and 5 , the gimbal unit assembly is attached by elastic bands 7 that wrap around strap support post 24 and are secured to hooks 16 by stopper knots 11 . the hooks 16 in turn are mounted on side blocks 1 that can be selectively positioned upwards or downwards on posts 2 . if desired , safety cables ( not shown ) can be attached between the hooks 16 and the end suspension assemblies 8 to prevent the elastic straps 7 from overextending or to protect the equipment in the event a strap 7 were to break . the posts 2 are connected to a cross rail 20 via gussets 22 which allow the posts 2 to be selectively positioned laterally along the cross rail 20 . the cross rail 20 is connected to a pair of bottom rails 19 by brackets 18 which are retained in grooves 4 . the bottom rails 19 may be selectively positioned fore - and - aft by adjusting the gussets 18 . the battery packs 14 for the gyroscopic stabilizers sit on the battery trays 12 and are secured via retaining straps 33 which are wrapped around the posts 2 . in operation , the bottom rails are secured to the aircraft or other mode of transport , generally within the compartment in which the pilot , driver , or passengers reside . for example , the bottom rails 19 may be attached to the seat rails of an aircraft . modes of attachment such as straps , clamps , and bolts can also be used to removably secure the mount to an aircraft , vehicle , or watercraft . the adjustability of the side blocks 1 , posts 2 , and bottom rails 19 allows for a high degree of flexibility with respect to adjusting the position of the gimbal unit assembly 51 relative to an opening or to the operator of the camera . the bearings 28 , 30 , 35 , and 42 are an important aspect of the mount because they enable smooth movement and refined control of the camera by the operator . of particular importance are bearings 42 in the end suspension assemblies 8 because they provide an unexpected degree of vibration damping over aerial photography mounts that utilize elastic suspension members to support the assembly to which the camera is fastened but which do not utilize independently - rotating bearings along the roll axis of rotation . the term bearings when used in this specification refers specifically to ball bearings or roller bearings . the bearings are preferably double - sealed , deep - groove ball bearings of the types commonly designated as 6200 - rs , 6201 - rs , and 99502h , although other types may be used . the elastic bands 7 can be made of any material that has sufficient elasticity to absorb vibration and sufficient tensile strength to support the gimbal assembly 51 when fitted with a camera , gyroscopic stabilizers 13 , and any counterweights . a particularly suitable form consists of cords made from multiple strands of elastic material , typically rubber , which are bound together by a woven nylon fabric covering . flat strap bungee material is readily available and also functions well . to handle heavier weight loads , the bands can be dual looped through the end suspension assemblies 8 and the hooks 16 . single and dual loop suspensions can be bound together with wire ties and then encapsulated with an industrial heat shrink tubing with adhesive coating on the inner diameter . alternative materials include premolded silicone bands which can be formed in different durometers to handle varying equipment weight combinations . tripod heads 5 are very useful in mounting cameras because they permit rapid and accurate adjustment so that the initial position of the camera may be preset to a desired degree of forward tilt . an example of a suitable head is the manfrotto model 460mg . gyroscopic stabilizers 13 are used to stabilize the movement about all three axes of rotation and can be adjustably positioned on the gyro mount plate 10 through the center lines of the respective axes . a suitable gyroscopic stabilizer for the mount is the model ks - 8 made by kenyon laboratories llc . further adjustments to the balance and center of gravity of the gimbal unit 51 can be made by moving and securing weights onto the gyro mount plate 10 . to operate the mount , the gyroscopic stabilizers 13 are activated and allowed to reach their operating rate of rotation . the gyroscopic stabilizers 13 exert a stabilizing effect along the axes of rotation and thus tend to restrain the camera from being jostled or incurring other inadvertent motion . the camera operator can direct the position of the camera by smoothly moving and aiming the camera with respect to the desired position . to facilitate control over the camera , the base mount plate 6 can be fitted with a handle 17 , as shown in fig5 , which the camera operator may hold and thus direct the position of the camera without touching the camera itself . it will be apparent to those skilled in the art that various modifications and variations can be made to the present invention without departing from its scope and spirit . thus , it is intended that the present invention covers the modifications and variations that come within the scope of the claims and their equivalents .