← Back to NASA Technology Projects
Terrain Relative Navigation (TRN) System for Landing Applications [SPLICE subsystem]
Completed
TRL 6 (started at 4, targeting 6)
Description
Draper’s Terrain Relative Navigation (TRN) System for Landing Applications is designed to provide precise vehicle navigation relative to a planetary body where GPS or ground updates are not readily available. Though algorithms for terrain relative navigation have been tested in ground applications for years, this technology addresses the need for reliable space-based systems. During a suborbital flight, the system successfully detected terrain features continuously while above an altitude of 330 feet. Images taken by an onboard camera were compared with a preloaded satellite map to identify common landmarks and track distinct features. This capability aims to improve a robotic or crewed lander’s knowledge of where there is a safe spot to touch down. Problem Statement The TRN system test apparatus is a self-contained, strapdown unit approximately 18”x12”x9” weighing ~4kg. Hardware includes an onboard BRIX computer, battery, sensor board (IMU, magnetometer, altimeter) and the optical camera. There are no required external interfaces. Telemetry will be available via onboard logging and broadcasted signal. Demonstrate capability of system to identify and provide accurate measurements of a set of known surface fixed features dependent on the current vehicle state. Demonstrate robustness of algorithm at various altitudes and light conditions (shadowing) via terrestrial flight testing on multiple vehicles. Technology Maturation The flight test demonstrated the capability of the system to fill a NASA need for technology that can successfully help lander vehicles navigate to safe landing locations for touch down. In addition, information gathered is enabling further hardware and algorithm evaluation, which is likely to result in updates targeting increased accuracy of estimated vehicle state.
Benefits
Draper’s TRN system provides a risk-reducing solution for space vehicle relative navigation. It is part of a suite of precision landing technologies for possible use on future lunar landers. This would benefit NASA missions and the commercial space industry. Future Customers • Continued development in NASA’s Safe and Precise Landing—Integrated Capabilities Evolution (SPLICE) project • Commercial lunar landers • NASA’s Artemis program
Details
| Technology area | Entry, Descent, and Landing > Flight Mechanics and GN&C for Entry, Descent, and Safe Precise Landing |
| Program | Flight Opportunities (FO) |
| Lead organization | The Charles Stark Draper Laboratory, Inc., Cambridge, MA |
| Start date | 2018-04-11 |
| End date | 2020-05-04 |
Project contacts
Listed on TechPort itself — the most direct way to ask about this specific project.
How to get involved
This is early/mid-stage (TRL 6) — the most realistic path in is NASA SBIR/STTR, which funds small businesses and research institutions to develop technology aligned with NASA's needs (equity-free, phased funding). Check whether a current SBIR/STTR solicitation topic overlaps with this project's technology area, or contact the project directly (above) to ask.
None of these are guaranteed paths for this specific project — TechPort itself doesn't have an "apply" button. Reaching out to the contact(s) above with a specific question is usually the fastest way to find out what's actually open.