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    • Home (overview)
    • Intro · what is cislunar space
    • Orbits · spacecraft trajectories
    • Frontiers · directions & labs
    • Glossary · terms & definitions
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  • Cislunar glossary (terms & definitions)

    • Cislunar Space Glossary
    • Fundamentals

      • Allan Deviation (ADEV)
      • Dual One-Way Ranging (DOWR)
      • Einstein Equivalence Principle (EEP)
      • Gravitational Redshift
      • High Altitude Airship (HAA)
      • Near-space
      • Passive Hydrogen Maser (PHM)
      • Stratospheric Airship
      • /en/glossary/fundamentals/absolute-range/
      • /en/glossary/fundamentals/aerodynamic-coefficient/
      • /en/glossary/fundamentals/aerodynamic-moment/
      • /en/glossary/fundamentals/aerospace-vehicle/
      • /en/glossary/fundamentals/ballistic-coefficient/
      • /en/glossary/fundamentals/bi-elliptic-transfer/
      • /en/glossary/fundamentals/body-frame/
      • /en/glossary/fundamentals/celestial-coordinate-system/
      • /en/glossary/fundamentals/celestial-sphere/
      • /en/glossary/fundamentals/characteristic-velocity/
      • /en/glossary/fundamentals/coverage-angle/
      • /en/glossary/fundamentals/earth-ellipsoid/
      • /en/glossary/fundamentals/earth-oblateness-perturbation/
      • /en/glossary/fundamentals/ecef-frame/
      • /en/glossary/fundamentals/energy-parameter/
      • /en/glossary/fundamentals/finite-thrust-maneuver/
      • /en/glossary/fundamentals/free-flight-phase/
      • /en/glossary/fundamentals/free-flight-trajectory/
      • /en/glossary/fundamentals/frozen-orbit/
      • /en/glossary/fundamentals/gaussian-perturbation-equations/
      • /en/glossary/fundamentals/geocentric-inertial-frame/
      • /en/glossary/fundamentals/gps-time/
      • /en/glossary/fundamentals/gravitational-potential/
      • /en/glossary/fundamentals/gravity-turn/
      • /en/glossary/fundamentals/gravity-vs-gravitation/
      • /en/glossary/fundamentals/hit-equation/
      • /en/glossary/fundamentals/hohmann-transfer/
      • /en/glossary/fundamentals/inertial-navigation-system/
      • /en/glossary/fundamentals/instantaneous-balance/
      • /en/glossary/fundamentals/isru/
      • /en/glossary/fundamentals/julian-date/
      • /en/glossary/fundamentals/kepler-equation/
      • /en/glossary/fundamentals/kompsat/
      • /en/glossary/fundamentals/lagrangian-perturbation-equations/
      • /en/glossary/fundamentals/launch-azimuth/
      • /en/glossary/fundamentals/launch-window/
      • /en/glossary/fundamentals/lift-to-drag-ratio/
      • /en/glossary/fundamentals/load-factor/
      • /en/glossary/fundamentals/longitudinal-lateral-motion/
      • /en/glossary/fundamentals/lunar-lander/
      • /en/glossary/fundamentals/minimum-energy-trajectory/
      • /en/glossary/fundamentals/newton-iteration-method/
      • /en/glossary/fundamentals/nutation/
      • /en/glossary/fundamentals/optimal-velocity-inclination/
      • /en/glossary/fundamentals/orbit-capture/
      • /en/glossary/fundamentals/orbit-insertion-conditions/
      • /en/glossary/fundamentals/orbital-elements/
      • /en/glossary/fundamentals/orbital-equation/
      • /en/glossary/fundamentals/orbital-maneuver/
      • /en/glossary/fundamentals/orbital-phase/
      • /en/glossary/fundamentals/orbital-transfer-vehicle/
      • /en/glossary/fundamentals/perturbation-motion/
      • /en/glossary/fundamentals/phasing-orbit/
      • /en/glossary/fundamentals/pitch-program/
      • /en/glossary/fundamentals/powered-phase/
      • /en/glossary/fundamentals/precession/
      • /en/glossary/fundamentals/pressure-center/
      • /en/glossary/fundamentals/range-error-coefficient/
      • /en/glossary/fundamentals/reentry-corridor/
      • /en/glossary/fundamentals/reentry-phase/
      • /en/glossary/fundamentals/repeat-ground-track-orbit/
      • /en/glossary/fundamentals/reusable-launch-vehicle/
      • /en/glossary/fundamentals/satellite-ring/
      • /en/glossary/fundamentals/sequential-quadratic-programming/
      • /en/glossary/fundamentals/skip-reentry/
      • /en/glossary/fundamentals/solar-exposure-factor/
      • /en/glossary/fundamentals/specific-angular-momentum/
      • /en/glossary/fundamentals/specific-impulse/
      • /en/glossary/fundamentals/stagnation-heat-flux/
      • /en/glossary/fundamentals/standard-atmosphere/
      • /en/glossary/fundamentals/subsatellite-track/
      • /en/glossary/fundamentals/sun-synchronous-orbit/
      • /en/glossary/fundamentals/thrust-to-weight-ratio/
      • /en/glossary/fundamentals/thrust/
      • /en/glossary/fundamentals/total-angle-of-attack/
      • /en/glossary/fundamentals/trajectory-equation/
      • /en/glossary/fundamentals/trajectory-optimization/
      • /en/glossary/fundamentals/trim-angle-of-attack/
      • /en/glossary/fundamentals/true-anomaly/
      • /en/glossary/fundamentals/tsiolkovsky-equation/
      • /en/glossary/fundamentals/turning-program/
      • /en/glossary/fundamentals/two-body-problem/
      • /en/glossary/fundamentals/utc/
      • /en/glossary/fundamentals/variation-of-parameters/
      • /en/glossary/fundamentals/velocity-frame/
      • /en/glossary/fundamentals/velocity-inclination-angle/
      • /en/glossary/fundamentals/vis-viva-equation/
      • /en/glossary/fundamentals/vleo/
      • /en/glossary/fundamentals/walker-constellation/
      • /en/glossary/fundamentals/zero-angle-of-attack-reentry/
    • Dynamics & Math

      • A* Search Algorithm (A* Search)
      • A2PPO (Attention-Augmented Proximal Policy Optimization)
      • Action-Angle Variables
      • Backstepping Sliding Mode Control
      • Backward Stability Set
      • Bang-bang Control (Bang-bang Control)
      • Barycentric Synodic Coordinate System
      • Batch Deployment (Batch Deployment)
      • Bicircular Four-Body Problem
      • Birkhoff-Gustavson Normal Form
      • Buoyancy-weight Imbalance
      • Capture Set
      • Central Manifold
      • Chaos Effect
      • Clohessy-Wiltshire (CW) Equation
      • Co-state Normalization (Co-state Normalization)
      • Coasting Arc (Coasting Arc)
      • Continuation Method (Parameter Continuation)
      • Continuation (延拓)
      • Cooperative Agent (CA)
      • CR3BP with Low-Thrust (CR3BP-LT)
      • Circular Restricted Three-Body Problem (CR3BP)
      • Curriculum Learning
      • Deep Reinforcement Learning
      • Differential Correction (微分修正)
      • Differential Evolution (DE) Algorithm
      • Differential Games (Differential Games)
      • Direct Collocation
      • Dynamic Programming (Dynamic Programming)
      • Dynamic Target Method
      • Ephemeris Model
      • Equinoctial Orbital Elements (Equinoctial Orbital Elements)
      • Fuzzy Backstepping Control
      • Generalized Advantage Estimation (GAE)
      • Gaussian Process Regression
      • Geocentric Rotating Coordinate System (GRC)
      • Heteroclinic Orbit Transfer (Heteroclinic Orbit Transfer)
      • Hill Three-Body Problem
      • Homotopy Method (Homotopy Method)
      • Improved Baseline Control-Point Method (Improved Baseline Control-Point Method)
      • Impulsive Maneuver (脉冲机动)
      • Initial Value Optimization
      • Invariant Manifold (Invariant Manifold)
      • J2000 Geocentric Equatorial Coordinate System (J2000 Geocentric Equatorial Coordinate System)
      • Jacobi Constant (Jacobi Integral)
      • K-Means Clustering (K-Means Clustering)
      • K-Medoids Clustering (K-Medoids Clustering)
      • KD-Tree (KD-Tree)
      • Libration Point (Equilibrium Point)
      • Libration Point Spacecraft Body Coordinate System (Libration Point Spacecraft Body Coordinate System)
      • Libration Point Spacecraft Orbital Coordinate System (Libration Point Spacecraft Orbital Coordinate System)
      • Lindstedt-Poincare Method (Lindstedt-Poincare Method)
      • L2-centered Rotating Coordinate System (L2-centered Rotating Coordinate System, LRC)
      • Low-Thrust Transfer MDP Formulation
      • Mass Discontinuity (Mass Discontinuity)
      • Monodromy Matrix
      • Newton-Euler Equations
      • Particle Swarm Optimization
      • Patch Point (Splicing Point)
      • Patched Method (拼接法)
      • Poincaré Map (庞加莱图)
      • Poincaré Section
      • Quasi-Bicircular Problem (QBCP)
      • Quasi-Bicircular Four-Body Problem
      • Regional Station-keeping Control
      • Seven-node Model
      • Shooting Method
      • Six-DOF Motion Equations
      • Sliding Mode Control
      • Solar Radiation Pressure (SRP)
      • Stability Index
      • Stability Set
      • State Transition Matrix (STM)
      • Static Lift
      • Strobe Map
      • Targeting Method
      • Thermo-mechanical Coupling Model
      • Thermodynamic Model
      • Two-Level Differential Correction Method
      • Two-node Model
      • Variational Mode Decomposition
      • Zero-Velocity Surface
      • /en/glossary/dynamics/ddpg/
      • /en/glossary/dynamics/hcpso/
      • /en/glossary/dynamics/mo-mcts/
      • /en/glossary/dynamics/nsga-ii/
      • /en/glossary/dynamics/pareto-optimal/
      • /en/glossary/dynamics/pontryagin-principle/
      • /en/glossary/dynamics/pseudo-arclength-continuation/
      • /en/glossary/dynamics/pursuit-evasion-game/
      • /en/glossary/dynamics/q-law/
      • /en/glossary/dynamics/reachable-set/
      • /en/glossary/dynamics/reduced-order-dynamics/
      • /en/glossary/dynamics/regularization/
      • /en/glossary/dynamics/rlepeso/
      • /en/glossary/dynamics/saddle-point-strategy/
      • /en/glossary/dynamics/state-dependent-tsp/
      • /en/glossary/dynamics/two-dominant-invariant-manifold/
      • /en/glossary/dynamics/zero-effort-miss/
    • Mission orbits

      • Apolune (远月点)
      • Ballistic Capture Orbit
      • Cycler Trajectory
      • DRO Constellation
      • Distant Retrograde Orbit (DRO)
      • Earth-Moon L1/L2 Halo Orbit (EML1/EML2 Halo)
      • Free-Return Trajectory (自由返回轨道)
      • Full Lunar Surface Coverage Orbit
      • Halo Orbit (Halo 轨道)
      • Lissajous Orbit (Lissajous 轨道)
      • Low-Energy Transfer Orbit
      • Lyapunov Orbit (Lyapunov 轨道)
      • Multi-Revolution Halo Orbit
      • Near-Rectilinear Halo Orbit (NRHO)
      • Orbit Identification
      • Orbit Keeping (Station-Keeping)
      • Parking Orbit (停泊轨道)
      • Perilune (近月点)
      • Prograde (顺行)
      • Quasi-Periodic Orbit
      • Resonance Orbit
      • Retrograde (逆行)
      • Transfer Orbit (转移轨道)
      • /en/glossary/orbits/axial-orbit/
      • /en/glossary/orbits/butterfly-orbit/
      • /en/glossary/orbits/dpo/
      • /en/glossary/orbits/horseshoe-orbit/
      • /en/glossary/orbits/hub-and-spoke/
      • /en/glossary/orbits/lopo/
      • /en/glossary/orbits/polynomial-constraint-stationkeeping/
      • /en/glossary/orbits/primary-impulse-transfer/
      • /en/glossary/orbits/vertical-orbit/
    • Navigation

      • Altitude Regulation
      • Cislunar Spatiotemporal Reference
      • Earth-Moon Hybrid Navigation
      • Earth GNSS Weak Signal Navigation
      • Inter-Satellite Link Navigation
      • LiAISON Navigation
      • LunaNet (Lunar Network)
      • Lunar Navigation Constellation
      • Moonlight Initiative
      • Tiandu-1
      • Trajectory Planning
      • X-ray Pulsar Navigation
      • /en/glossary/navigation/autonomous-navigation/
      • /en/glossary/navigation/extended-kalman-filter/
      • /en/glossary/navigation/gagan/
      • /en/glossary/navigation/irnss/
      • /en/glossary/navigation/observability/
      • /en/glossary/navigation/orbit-identification/
      • /en/glossary/navigation/pnt/
      • /en/glossary/navigation/sem-autonomous-navigation/
    • Lunar minerals

      • Changeite-Ce (Cerium Changeite)
      • Changeite-Mg (Magnesium Changeite)
    • Programs & missions

      • Artemis Program
      • LuGRE Experiment
    • Other

      • Actuator Error
      • Chain-of-Thought (CoT) Prompting
      • Cislunar Navigation Prospects
      • Cislunar Space (地月空间)
      • EXOSIMS
      • Floquet Mode Method
      • Impulse Thrust
      • Insertion Error
      • Low Earth Orbit / LEO (低地球轨道)
      • Low-Rank Adaptation (LoRA)
      • Lunar Gravity Assist / LGA (月球借力)
      • Navigation Error
      • Noncooperative Target
      • Nuclear Thermal Propulsion (NTP)
      • Orbit Insertion (入轨)
      • Period-Doubling Bifurcation
      • Longitudinal Coupling Vibration (POGO)
      • Powered Lunar Flyby / PLF (有动力月球借力)
      • Prompt Tuning (P-tuning)
      • Reflection Coefficient (C_R)
      • Solar Constant (S₀)
      • Space Traffic Management (STM)
      • Spacecraft Intention Recognition
      • Starshade
      • Weak Stability Boundary / WSB (弱稳定边界)
      • /en/glossary/other/gslv/
      • /en/glossary/other/insat/
      • /en/glossary/other/orbital-residence-platform/
      • /en/glossary/other/pslv/
      • /en/glossary/other/pursuit-evasion-defense/
    • Organizations

      • Anduril Industries
      • Booz Allen Hamilton
      • General Dynamics Mission Systems
      • GITAI USA
      • Lockheed Martin
      • Northrop Grumman
      • Quindar
      • Raytheon Missiles & Defense
      • Sci-Tec
      • SpaceX
      • True Anomaly
      • Turion Space
      • /en/glossary/organizations/danuri/
      • /en/glossary/organizations/isro/
      • /en/glossary/organizations/kasa/
      • /en/glossary/organizations/sriharikota/
      • /en/glossary/organizations/true-anomaly-company/
    • Military space doctrine

      • Cislunar Space Situational Awareness
      • Competitive Endurance
      • Component Field Commands
      • Commander, Space Forces (COMSPACEFOR)
      • Counterspace Operations
      • DOTMLPF-P Framework
      • Force Design
      • Force Development
      • Force Employment
      • Force Generation
      • Golden Dome
      • Mission Command
      • Mission Delta (MD)
      • Operational Test and Training Infrastructure (OTTI)
      • Resilient/Disaggregated Architecture
      • Space Domain Awareness (SDA)
      • Space Mission Task Force (SMTF)
      • Space Superiority
      • Space Force Generation Process (SPAFORGEN)
      • System Delta (SYD)
      • /en/glossary/doctrine/asat/
      • /en/glossary/doctrine/civil-military-integration/
      • /en/glossary/doctrine/directed-energy-weapon/
      • /en/glossary/doctrine/distributed-architecture/
      • /en/glossary/doctrine/kinetic-weapon/
      • /en/glossary/doctrine/persistent-detection-corridor/
      • /en/glossary/doctrine/resilience-map/
    • Observation techniques

      • Astrometry
      • Background Star Elimination
      • Cislunar Moving Objects
      • Continuous Coverage (CP)
      • Earth Albedo
      • Ephemeris Correlation
      • Hot Pixel
      • Image Registration
      • Image Stacking
      • Lunar Glare Zone
      • Quasi-zero Wind Layer
      • Segmentation Map
      • Shift-and-Add (SAA)
      • Sidereal Tracking
      • Signal-to-Noise Ratio (SNR)
      • Solar Radiation
      • Source Extraction
      • Synthetic Tracking
      • Zonal Wind
      • /en/glossary/observation/illumination-constraint/
      • /en/glossary/observation/pointing-constraint/
    • Satellite Communication & TT&C

      • All-Time Seamless Communication
      • BeiDou Satellite System
      • Constellation Networking
      • Inter-Satellite Link (ISL)
      • Laser-Microwave Communication
      • Microwave Link

Sci-Tec

Author: 天疆说

Source: Public sources

Site: https://cislunarspace.cn

Company Overview

Sci-Tec is a U.S. aerospace sensor and instrument company specializing in the research, development, and manufacturing of satellite payloads, space exploration instruments, and navigation sensors. Sci-Tec has long-standing expertise in space science instruments such as star trackers, sun sensors, magnetometers, and spectrometers, providing sensor system solutions for NASA and commercial satellite operators. The company is mid-sized and has a strong technical reputation in the high-precision attitude determination optical sensor niche market.

Space and Cislunar-Related Business

Attitude Determination Sensors

Sci-Tec develops and produces multiple sensors for satellite attitude determination:

  • Star Tracker: Sci-Tec's star trackers are commonly used attitude determination devices on commercial and scientific satellites, achieving high-precision pointing (typically better than 1 arcsecond) through star pattern recognition. Star trackers are core instruments for maintaining attitude stability for all types of cislunar spacecraft.
  • Sun Sensor: Used to determine a satellite's orientation relative to the Sun, serving as an important backup sensor for attitude control systems.
  • Inertial Reference Unit (IRU): Provides high-precision angular rate and acceleration measurements, supporting satellite attitude control.

Scientific Payloads

  • Spectrometers and Imagers: Sci-Tec provides optical payloads for NASA's Earth observation satellites and deep space probes, used for scientific missions such as atmospheric composition analysis and surface mineral identification.
  • Occultation Measurement Instruments: Participated in NASA ozone monitoring and other scientific missions, providing high-precision optical path measurement instruments.

Potential Applications in Cislunar Navigation

Sci-Tec's navigation sensors have the following potential applications in the cislunar space environment:

  • High-Autonomy Navigation: Cislunar space lacks GNSS signals; high-precision star trackers and IRUs are core components for autonomous navigation of cislunar spacecraft.
  • Translunar Orbit Determination: Star trackers can still observe star patterns normally during lunar transfer orbits, enabling high-precision determination of translunar transfer orbits.

Major Products and Technologies

Product/TechnologyTypeDescription
Star TrackerAttitude SensorHigh-precision attitude determination, with sub-arcsecond accuracy
Sun SensorAttitude SensorSun direction detection, attitude backup
Inertial Reference UnitInertial MeasurementAngular rate and acceleration measurement
SpectrometerScientific InstrumentAtmospheric composition analysis and surface mineral identification
Magnetic Field Measurement InstrumentScientific InstrumentSpace plasma and magnetic field observation

Connection to Cislunar Space Missions

Sci-Tec's importance in the cislunar space domain lies in the critical supporting role of its navigation sensors:

  • High-Precision Attitude Control: Cislunar space missions (such as Gateway docking operations and translunar transfer orbit corrections) require high-precision attitude control; Sci-Tec's star trackers are fundamental to achieving this capability.
  • Autonomous Navigation: Communication delays in cislunar space make real-time ground control difficult; high-autonomy navigation sensors are a necessary condition for cislunar space probes to achieve autonomous flight.
  • Scientific Observation: Special observation platforms in cislunar space (such as lunar farside radio observatories and Lagrange point observatories) require high-precision attitude control and high-sensitivity sensors; Sci-Tec's products can meet such needs.

Related Terms

  • Cislunar Navigation Prospects: /en/glossary/other/cislunar-navigation-prospects/
  • Near-Rectilinear Halo Orbit: /en/glossary/orbits/nrho/

References

  • NASA Goddard, "Commercial sensor providers for satellite missions", 2024.
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Last Updated: 4/26/26, 5:34 PM
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