AAWSAP DIRD, Cockpits in the Era of Breakthrough Flight, November 2010
DOW-UAP-D144 · page 3 of 57
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UNCLASSIFIED/,'FOR OFFI@IAL WSE ONLY Contents Introduction ...........................................................................................................iv Chapter 1: Predicting Implications of Propulsion Breakthroughs ........................... 1 MARCH OF PROGRESS: REVOLUTIONARY PROPULSION PHYSICS....................... 1 VEHICLE and COCKPIT IMPLICATIONS............................................................... 2 Chapter 2: Human-Machine Interface Lessons ..................................................... 18 HUMAN PERCEPTION NORMS ........................................................................... 18 DESIGN FOR STRESS ............................................ ................................................. 21 DEVICES TO CONVEY INFORMATION ................................................................ 23 DEVICES FOR RECEIVING PILOT COMMANDS ................................................... 27 CONTEMPORARY AIRCRAFT COCKPITS............................................................. 28 Chapter 3: Provisional Cockpit for Breakthrough Flight........................................ 32 FLIGHT MODES ................................................................................................. 32 PHYSICAL DISPLAVS ........................................................................................ 34 VIRTUAL SURROUND DISPLAY ......................................................................... 40 CONTROLS ........................................................................................................ 41 Chapter 4: Future Work ........................................................................................ 43 MULTIPLE FLIGHT REGI ME GUIDANCE CONVENTIONS ..................................... 43 VECTOR MOTION DISPLAY ............................................................................... 43 VECTOR MOTION CONTROL .............................................................................. 43 OPTIMUM MIX OF CONTROL METHODS ............................................................. 44 Appendix A: Annotated Bibliography .................................................................... 45 Appendix B: Endnotes .......................................................................................... SO Figures Figure 1. Six Independent Degrees of Freedom...................................................... 3 Figure 2. Comparing Conventions of Aircraft Motion .............................................. 5 UNCLASSIFIED/ fFOA. OFFICIO Is. flili Ol'lls.¥ ii