Documents / Official release

AAWSAP DIRD, Cockpits in the Era of Breakthrough Flight, November 2010

U.S. Department of War · 2010-11-01 · 57 pages · text from the file's own layer

This Defense Intelligence Reference Document, dated 1 November 2010 and numbered DIA-08-1011-002, was prepared by the Defense Intelligence Agency's Defense Warning Office. It is one of a series of advanced technology reports produced under the Advanced Aerospace Weapon System Applications program. It draws mainly on the book Frontiers of Propulsion Science and speculates about breakthroughs such as control of gravity and inertia and faster-than-light travel. It then proposes a provisional cockpit design with six-degree-of-freedom controls, virtual displays and no windows.

From the source:Release of 2026-09-18 Incident: 11/1/10, Las Vegas, Nevada. Released with redactions. This document is a Defense Intelligence Reference Document (DIRD), a technical reference format used by the Defense Intelligence Agency (DIA) to capture baseline knowledge on a specific topic for later analytic use. DIRDs are best understood as reference and synthesis products rather than as original research. It is one of 38 DIRDs produced under the Advanced Aerospace Weapon System Applications Program (AAWSAP) between 2009 and 2011. Because AAWSAP’s scope permitted a broad range of supporting topics, not every DIRD in the series directly concerns aerospace systems or future threat assessment. The following summary reflects the DIRD’s scope and framing at the time of writing and should not be read as implying current validation of the concepts discussed. This DIRD examines how cockpit design might change if future aerospace vehicles were ever to achieve major propulsion breakthroughs such as control over gravity and inertia, “propellantless” flight, or faster-than-light travel. The report does not describe an existing or emerging vehicle class. Instead, it asks what such hypothetical capabilities would mean for piloting, displays, controls, and human factors, and it argues that the biggest design challenges would come from full six-degree-of-freedom motion, operation across multiple flight regimes from near-surface flight to orbit and deep space, and the possible separation between the craft’s actual motion and the crew’s internal physical sensations. It combines those assumptions with established human-machine-interface principles and with maturing inputs such as gesture, voice, and brain-machine control to outline a provisional cockpit centered on intuitive displays, stress-tolerant physical controls, and a virtual surround display.

  • p. 2 …a series of advanced technology reports produced in FY 2009 under the Defense Intelligence Agency, Defense…
  • p. 5 …How these advances may affect future cockpits is described, and this is the central message of…
  • p. 6 …the far future, this study evaluates the impact of having achieved the following breakthrough advancements: • Control…
  • p. 12 …then contemplate the consequences that these advances impose onto other systems of the vehicle-in this…
  • p. 21 …In support of the forgoing discussion, we are speculating that heretofore unknown advances in physics regarding…
  • p. 32 …As evidenced by the gaming industry, the motions of the pilot's hands-whether by a…
  • p. 44 …advances in sensor technology might provide other abilities that are not yet foreseeable . Following the requirements…
  • p. 45 …Taking advantage of foreseeable advances, such images are likely to be in the form of virtual…
  • p. 48 …advances in cockpits for breakthrough flight might be further advanced by taking advantage of the gaming…
  • p. 51 …on an advanced version or next generation of heads-up display to outline the road, pinpoint…
  • p. 53 …Regard less of such advances, the keyboard is still likely to be around for those lingering…
  • p. 55 …Methods in the first 6 rows of t hat table would not require the double hull…
UNCLASSIFIED/ ,'FOR OFFI@IAI:: ~SE OPtl::Y
Both side panels are deliberately not in the tunnel vision zone, since they provide
add it iona l functions that are less time critical. Each side panel is a mix of fixed and
adaptive displays. The convention is that the panel on the left (consistent with the
navigation panel on the left) is for displays and controls related to the envi ronment
outside the craft, while the panel on the right is associated with the function of the craft
itself.
Only some of the sensors and functions are known at this time, and it is expected that
fu rther advances in sensor technology might provide other abilities that are not yet
foreseeable . Following the requirements from Chapter 1, this panel will at least have
controls for the fol lowing :
• External visible spectrum cameras that provide input to the virtual surround display .
• Augmented spectrum cameras (e.g., infrared or ultraviolet).
• Star tracker.
• Cosmic microwave background sensors.
• Inertial sensors and their related integrations for velocity and position.
• Object detection and trajectory determination.
Internal Conditions Panel
The right panel flanking the pilot seat has more detailed displays and controls regarding
the vehicle's functions, such as energy, propulsion, and computation. Similar to the left
side panel, it is a mix of fixed and adaptive displays.
This panel provides deeper levels of detail for the elements displayed on the vehicle
status panel, along with control settings for the same. The functions of this panel are
closely integrated with the flight-assist system, especially in regard to recommending
corrective actions to vehicle malfunctions.
Absent the technology for the vehicle's breakthrough propulsion and power systems,
further details of this panel cannot be suggested at this time.
Periphery Motion Displays
The last two physical panels are the periphery motion displays, which are located on
either side of the cockpit in the pilot's periphery vision. They are a physical back-up to
the virtual surround display, where each offers more intense moving grid lines.
The panels simply display a grid whose motion is synced with the motion of the craft
relative to the surrounding space. In this way, the pilot gets subtle cues to motions
that can be mentally processed in parallel with the other displays. Such an additional
motion display is expected to become necessary because of the added degrees of
freedom available for the vehicle's motion. This can be particularly useful during hover,
UNCLASSIFIED/,<FOA. OFFICIO ls Plili ONI.¥
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Official release, from the pursue collection. The PDF is mirrored here; the original link is above. 57 pages are in the text index: search them above, or from the library's search.