NASA Logo

NTRS

NTRS - NASA Technical Reports Server

Back to Results
Developing a Prototype ALHAT Human System Interface for LandingThe goal of the Autonomous Landing and Hazard Avoidance Technology (ALHAT) project is to safely execute a precision landing anytime/anywhere on the moon. This means the system must operate in any lighting conditions, operate in the presence of any thruster generated regolith clouds, and operate without the help of redeployed navigational aids or prepared landing site at the landing site. In order to reach this ambitious goal, computer aided technologies such as ALHAT will be needed in order to permit these landings to be done safely. Although there will be advanced autonomous capabilities onboard future landers, humans will still be involved (either onboard as astronauts or remotely from mission control) in any mission to the moon or other planetary body. Because many time critical decisions must be made quickly and effectively during the landing sequence, the Descent and Landing displays need to be designed to be as effective as possible at presenting the pertinent information to the operator, and allow the operators decisions to be implemented as quickly as possible. The ALHAT project has established the Human System Interface (HSI) team to lead in the development of these displays and to study the best way to provide operators enhanced situational awareness during landing activities. These displays are prototypes that were developed based on multiple design and feedback sessions with the astronaut office at NASA/ Johnson Space Center. By working with the astronauts in a series of plan/build/evaluate cycles, the HSI team has obtained astronaut feedback from the very beginning of the design process. In addition to developing prototype displays, the HSI team has also worked to provide realistic lunar terrain (and shading) to simulate a "out the window" view that can be adjusted to various lighting conditions (based on a desired date/time) to allow the same terrain to be viewed under varying lighting terrain. This capability will be critical to determining the effect of terrain/lighting on the human pilot, and how they use windows and displays during landing activities. The Apollo missions were limited to about 28 possible launch days a year due to lighting and orbital constraints. In order to take advantage of more landing opportunities and venture to more challenging landing locations, future landers will need to utilize sensors besides human eyes for scanning the surface. The ALHAT HSI system must effectively convey ALHAT produced information to the operator, so that landings can occur during less "optimal" conditions (lighting, surface terrain, slopes, etc) than was possible during Apollo missions. By proving this capability, ALHAT will simultaneously provide more flexible access to the moon, and greater safety margins for future landers. This paper will specifically focus on the development of prototype displays (the Trajectory Profile Display (TPD), Landing Point Designation (LPD), and Crew Camera View (CCV) ), implementation of realistic planetary terrain, human modeling, and future HSI plans.
Document ID
20110002859
Document Type
Conference Paper
Authors
Hirsh, Robert L. (NASA Johnson Space Center Houston, TX, United States)
Chua, Zarrin K. (Georgia Inst. of Tech. Atlanta, GA, United States)
Heino, Todd A. (NASA Johnson Space Center Houston, TX, United States)
Strahan, Al (NASA Johnson Space Center Houston, TX, United States)
Major, Laura (Draper (Charles Stark) Lab., Inc. Cambridge, MA, United States)
Duda, Kevin (Draper (Charles Stark) Lab., Inc. Cambridge, MA, United States)
Date Acquired
August 25, 2013
Publication Date
January 1, 2011
Subject Category
Spacecraft Instrumentation and Astrionics
Report/Patent Number
JSC-CN-22512
IEEEAC Paper No. 1443
Meeting Information
IEEE Aerospace Conference(Big Sky, MT)
Funding Number(s)
WBS: WBS 079749.01.10
Distribution Limits
Public
Copyright
Other