Seeker (spacecraft)
 The Seeker spacecraft (lower left) and the Kenobi communications relay | |
| Manufacturer | NASA |
|---|---|
| Country of origin | United States |
| Operator | NASA |
| Applications | in-space inspection |
| Specifications | |
| Spacecraft type | Automated free-flying inspector |
| Bus | custom 3U |
| Dry mass | ~4kg[1] |
| Dimensions | 30cm x 10cm x 10cm[1] |
| Design life | ~40 minute mission[1] |
| Production | |
| Status | mission complete |
| On order | 0 |
| Built | 1 |
| Launched | 1 |
| Operational | 0 |
| Lost | 0 |
| Maiden launch | 17 April 2019 |
| Last launch | 17 April 2019 |
| Related spacecraft | |
| Derived from | Mini AERCam |
| Flown with | Cygnus |
 | |
Seeker is a NASA CubeSat intended to demonstrate ultra-low cost in-space inspection capability. Taken from design to delivery from late 2017 to early 2019, Seeker was launched on board the Cygnus NG-11 mission. Seeker deployed and operated around Cygnus on September 16, 2019.[2]
The Seeker free-flyer is a 3U CubeSat, approximately 30cm by 10cm by 10cm and weighing 4kg. It uses a cold-gas propulsion system with additively manufactured components, GPS, laser rangefinder, neural networks to drive a vision-based navigation system, Wi-Fi communication, and commercial off-the-shelf (COTS) parts wherever possible. The spacecraft is paired with a communications relay, called Kenobi, that provides an interface to the Cygnus vehicle. The spacecraft is design to be as automated as possible, requiring minimal input from the ground in order to complete its mock inspection mission.[1][3][4][5][6][7][8]
Avionics
[edit]Seeker's flight software (FSW) is run on a CHREC Space Processor. An Intel Joule is used for the computationally-intensive vision-based navigation algorithms. Seeker's propulsion system is controlled by a custom, FPGA-based board and power is provided to the system from GomSpace NanoPower BP4 batteries.[1]
Propulsion
[edit]The Seeker vehicle contained a small 6 – Degree of Freedom, cold gas nitrogen based cubesat propulsion system. The propulsion system is approximately 1.25U in size and contains 12 0.1 N thrusters. The system contained a small titanium pressure vessel and was capable of providing approximately 5 m/s DV.[9]
In an effort to minimize mass, optimize packing, and substantial reductions in iteration time between designs, a significant effort was undertaken to utilize additive manufacturing (AM) technology as part of the Seeker propulsion system. The certified AM thrusters were the first known additively manufactured (AM) pressurized plastic components which are designed to meet or exceed NASA standards and are certified for pressurized ground and flight use around operators.[10]
Guidance, navigation, and control system
[edit]Automated Flight Manager
[edit]Seeker's Automated Flight Manager (AFM) is a FSW application that allows the vehicle to function highly independently of human input. The AFM is a state machine that ensures the vehicle's systems are in the appropriate configuration for each phase of the mission.[1]
Navigation
[edit]Seeker's navigation system consists of two core FSW applications and six applications that provide appropriately processed sensor information. The system leverages Project Morpheus architecture and code components. The core of the navigation system is a propagator that integrates the vehicle state at 50 Hz and a multiplicative extended kalman filter that updates the state at 5Hz.[1]
Guidance
[edit]Seeker's guidance FSW application ran at 5Hz and allowed for waypoint seeking, position and attitude holds, target tracking, and limited Seeker's kinetic energy by limiting the vehicle's overall velocity.[1]
Control
[edit]Seeker's control FSW application ran at 5Hz and calculated translational commands with a proportional-integral function and rotational commands with a phase plane function. The application then combined these inputs into a single command that accounted for thruster limitations.[1]
Sensors
[edit]Seeker's sensor suite consisted of a STIM-300 IMU, a DLEM-SR laser rangefinder, a camera feeding the vision-based navigation system, GPS, and nanoSSOC-D60 Sun sensors.[1]
Vision-based Navigation System
[edit]The UT Austin Texas Spacecraft Laboratory developed an algorithm that processed images taken by the Seeker camera into bearing measurements by identifying the Cygnus with a convolutional neural network and then using a traditional computer vision approach to centroid it. This approach was found to be more robust than purely traditional alternatives in ground testing.[2][1]
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Neural network bounding Cygnus against a dark background -
Neural network bounding Cygnus with Earth in the background
Mission Results
[edit]Seeker deployed from Cygnus on September 19, 2019 and gathered the below images (stitched together into a gif).
See also
[edit]References
[edit]- ^ a b c d e f g h i j k Seeker Free-Flying Inspector GNC System Overview, February 2019. Retrieved in July 2019.
- ^ a b "Seeker". Texas Spacecraft Laboratory. Retrieved December 4, 2022.
- ^ Project Seeker, April 17, 2019. Retrieved in July 2019.
- ^ Seek(er) and NASA shall find, October 23, 2018. Retrieved in July 2019.
- ^ NTRS 20170003835, 2017. Retrieved in July 2019.
- ^ TSL Seeker, 2019. Retrieved in July 2019.
- ^ NASA Seeker Robot, April 17, 2019. Retrieved in July 2019.
- ^ Seeker 1.0: Prototype Robotic FreeFlyingInspector Mission Overview , Retrieved in October 2019.
- ^ Radke, Christopher D.; Atwell, Matthew; Studak, Bill (August 16, 2019). "Design, Development, and Certification, of the Seeker Robotic Free Flier Propulsion System". AIAA Propulsion and Energy 2019 Forum (Report). AIAA. doi:10.2514/6.2019-3956. ISBN 978-1-62410-590-6. Retrieved December 4, 2022.
- ^ "The Technology House produces NASA-certified, high-performance parts with the Carbon DLS™ process". Carbon3D.com. Retrieved December 4, 2022.
- This article incorporates text in the public domain from NASA, an agency of the United States government.