The conceptual design for converting the vertical motion simulator (VMS) to a multi-purpose aircraft and helicopter simulator is presented. A unique, high performance four degrees of freedom (DOF) motion system was developed to permanently replace the present six DOF synergistic system. The new four DOF system has the following outstanding features: (1) will integrate with the two large VMS translational modes and their associated subsystems; (2) can be converted from helicopter to fixed-wing aircraft simulation through software changes only; (3) interfaces with an advanced cab/visual display system of large dimensions; (4) makes maximum use of proven techniques, convenient materials and off-the-shelf components; (5) will operate within the existing building envelope without modifications; (6) can be built within the specified weight limit and avoid compromising VMS performance; (7) provides maximum performance with a minimum of power consumption; (8) simple design minimizes coupling between motions and maximizes reliability; and (9) can be built within existing budgetary figures.
Feasibility and concept study to convert the NASA/AMES vertical motion simulator to a helicopter simulator
1978-09-01
Report
No indication
English
Brown-Out Symbology Simulation (BOSS) on the NASA Ames Vertical Motion Simulator
British Library Conference Proceedings | 2008
|Design of a Hexapod Motion Cueing System for the NASA Ames Vertical Motion Simulator
British Library Conference Proceedings | 2002
|