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    • Home (overview)
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  • Cislunar glossary (terms & definitions)

    • Cislunar Space Glossary
    • Fundamentals

      • Absolute Range
      • Aerodynamic Coefficient
      • Aerodynamic Moment
      • Aerospace Vehicle
      • Allan Deviation (ADEV)
      • Ballistic Coefficient
      • Bi-Elliptic Transfer
      • Body Frame
      • Celestial Coordinate System
      • Celestial Sphere
      • Characteristic Velocity
      • Coverage Angle
      • Dual One-Way Ranging (DOWR)
      • Earth Ellipsoid
      • Earth Oblateness Perturbation
      • Earth-Centered Earth-Fixed Frame (ECEF)
      • Einstein Equivalence Principle (EEP)
      • Energy Parameter
      • Earth Observation (EO)
      • Finite Thrust Maneuver
      • Free-Flight Phase
      • Free-Flight Trajectory
      • Frozen Orbit
      • Gaussian Perturbation Equations
      • Geocentric Inertial Frame
      • GPS Time
      • Gravitational Potential
      • Gravitational Redshift
      • Gravity Turn
      • Gravity vs Gravitation
      • High Altitude Airship (HAA)
      • Hit Equation
      • Hohmann Transfer
      • Inertial Navigation System
      • Instantaneous Balance Assumption
      • In-Situ Resource Utilization (ISRU)
      • Julian Date
      • Kepler's Equation
      • Korea Multi-Purpose Satellite (KOMPSAT)
      • Lagrangian Perturbation Equations
      • Launch Azimuth
      • Launch Window
      • Lift-to-Drag Ratio
      • Load Factor
      • Longitudinal and Lateral Motion
      • Lunar Lander
      • Minimum Energy Trajectory
      • Near-space
      • Newton's Iteration Method
      • Nuri (KSLV-II)
      • Nutation
      • Optimal Velocity Inclination
      • Orbit Capture
      • Orbit Insertion Conditions
      • Orbital Elements
      • Orbital Equation
      • Orbital Maneuver
      • Orbital Phase
      • Orbital Transfer Vehicle
      • Passive Hydrogen Maser (PHM)
      • Perturbation Motion
      • Phasing Orbit
      • Pitch Program Angle
      • Powered Phase
      • Precession
      • Center of Pressure
      • Range Error Coefficient
      • Reentry Corridor
      • Reentry Phase
      • Repeat Ground Track Orbit
      • Reusable Launch Vehicle
      • Synthetic Aperture Radar (SAR)
      • Satellite Ring
      • Sequential Quadratic Programming
      • Skip Reentry
      • Solar Exposure Factor
      • Specific Angular Momentum
      • Specific Impulse
      • Stagnation Heat Flux
      • Standard Atmosphere
      • Stratospheric Airship
      • Subsatellite Track
      • Sun-Synchronous Orbit
      • Thrust-to-Weight Ratio
      • Thrust
      • Total Angle of Attack
      • Trajectory Equation
      • Trajectory Optimization
      • Trim Angle of Attack
      • True Anomaly
      • Tsiolkovsky Rocket Equation
      • Powered Phase Turning Process
      • Two-Body Problem
      • Coordinated Universal Time
      • Variation of Parameters
      • Velocity Frame
      • Velocity Inclination Angle
      • Vis-Viva Equation
      • Very Low Earth Orbit (VLEO)
      • Walker Constellation
      • 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)
      • Co-state Variables
      • Coasting Arc (Coasting Arc)
      • Continuation Method (Parameter Continuation)
      • Continuation
      • Cooperative Agent (CA)
      • CR3BP with Low-Thrust (CR3BP-LT)
      • Circular Restricted Three-Body Problem (CR3BP)
      • Curriculum Learning
      • Deep Deterministic Policy Gradient (DDPG)
      • Deep Reinforcement Learning
      • Detection Graph
      • Differential Correction
      • 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)
      • Earth Restricted Three-Body Problem (ERTBP)
      • Fuel-optimal Control
      • Fuzzy Backstepping Control
      • Generalized Advantage Estimation (GAE)
      • Gaussian Process Regression
      • Geocentric Rotating Coordinate System (GRC)
      • Hamiltonian
      • Hybrid Cluster Particle Swarm Optimization (HCPSO)
      • 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
      • 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)
      • LSTM Neural Network
      • Low-Thrust Transfer MDP Formulation
      • Mass Discontinuity (Mass Discontinuity)
      • Multi-Objective Monte Carlo Tree Search (MO-MCTS)
      • Modal Analysis
      • Monodromy Matrix
      • Monte Carlo Tree Search
      • Newton-Euler Equations
      • NSGA II (Non-dominated Sorting Genetic Algorithm II)
      • Pareto Optimality
      • Particle Swarm Optimization
      • Patch Point (Splicing Point)
      • Patched Method
      • Poincaré Map
      • Poincaré Section
      • Pontryagin's Maximum Principle
      • Pseudo-Arclength Continuation
      • Spacecraft Pursuit-Evasion Game
      • Q-Law Control Law
      • Quasi-Bicircular Problem (QBCP)
      • Quasi-Bicircular Four-Body Problem
      • Reachable Set
      • Reduced-Order Dynamic Equations
      • Regional Station-keeping Control
      • Regularization
      • Reinforcement Learning Enhanced Particle Swarm Optimization (RLEPSO)
      • Saddle-Point Strategy
      • Seven-node Model
      • Shooting Method
      • Six-DOF Motion Equations
      • Sliding Mode Control
      • Solar Radiation Pressure (SRP)
      • Stability Index
      • Stability Set
      • State-Dependent Traveling Salesman Problem (SDTSP)
      • State Transition Matrix (STM)
      • Static Lift
      • Strobe Map
      • Switching Function
      • Targeting Method
      • Thermo-mechanical Coupling Model
      • Thermodynamic Model
      • Two-Point Boundary Value Problem (TPBVP)
      • Trim Condition
      • Two-Dominant Invariant Manifold Method
      • Two-Level Differential Correction Method
      • Two-node Model
      • Variational Mode Decomposition
      • Zero-Effort Miss (ZEM)
      • Zero-Velocity Surface
    • Mission orbits

      • Apolune
      • Axial Orbit
      • Ballistic Capture Orbit
      • Butterfly Orbit
      • Cycler Trajectory
      • Distant Prograde Orbit (DPO)
      • DRO Constellation
      • Distant Retrograde Orbit (DRO)
      • Earth-Moon L1/L2 Halo Orbit (EML1/EML2 Halo)
      • Free-Return Trajectory
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      • Long Period Orbit
      • Low Prograde Orbit (LoPO)
      • Low-Energy Transfer Orbit
      • Low-Thrust Transfer Orbit
      • Lyapunov Orbit
      • Multi-Revolution Halo Orbit
      • Near-Rectilinear Halo Orbit (NRHO)
      • Orbit Identification
      • Orbit Keeping (Station-Keeping)
      • Parking Orbit
      • Perilune
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      • Primary Impulse Orbit Transfer
      • Prograde
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      • Resonance Orbit
      • Retrograde
      • Short Period Orbit
      • Transfer Orbit
      • Triangular Libration Points
      • Vertical Orbit
    • Navigation & systems

      • Altitude Regulation
      • Autonomous Navigation
      • Cislunar Spatiotemporal Reference
      • Earth-Moon Hybrid Navigation
      • Extended Kalman Filter (EKF)
      • GPS Aided GEO Augmented Navigation (GAGAN)
      • Earth GNSS Weak Signal Navigation
      • Inter-Satellite Link Navigation
      • Indian Regional Navigation Satellite System (IRNSS)
      • LEO Navigation Augmentation
      • LiAISON Navigation
      • LunaNet (Lunar Network)
      • Lunar Navigation Constellation
      • Moonlight Initiative
      • Observability
      • Positioning, Navigation, and Timing (PNT)
      • Sun-Earth-Moon Autonomous Navigation
      • Tiandu-1
      • Trajectory Planning
      • X-ray Pulsar Navigation
    • Astronomy & observation

      • Astrometry
      • Background Star Elimination
      • Cislunar Moving Objects
      • Continuous Coverage (CP)
      • Earth Albedo
      • Ephemeris Correlation
      • Hot Pixel
      • Illumination Constraint
      • Image Registration
      • Image Stacking
      • Infrared Radiation
      • Lunar Glare Zone
      • Pointing Constraint
      • 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
    • Military space doctrine

      • Anti-Satellite Test (ASAT)
      • Cislunar Space Situational Awareness
      • Civil-Military Integration
      • Competitive Endurance
      • Component Field Commands
      • Commander, Space Forces (COMSPACEFOR)
      • Counterspace Operations
      • Directed Energy Weapon (DEW)
      • Distributed Architecture
      • DOTMLPF-P Framework
      • Force Design
      • Force Development
      • Force Employment
      • Force Generation
      • Golden Dome
      • Kinetic Weapon
      • Mission Command
      • Mission Delta (MD)
      • Operational Test and Training Infrastructure (OTTI)
      • Persistent Detection Corridor (PDC)
      • Resilience Map
      • Resilient/Disaggregated Architecture
      • Space Domain Awareness (SDA)
      • Space Mission Task Force (SMTF)
      • Space Superiority
      • Space Force Generation Process (SPAFORGEN)
      • System Delta (SYD)
    • Organizations

      • Anduril Industries
      • Booz Allen Hamilton
      • Danuri Lunar Orbiter
      • General Dynamics Mission Systems
      • GITAI USA
      • Indian Space Research Organisation
      • Korea Aerospace Administration
      • Lockheed Martin
      • Northrop Grumman
      • Quindar
      • Raytheon Missiles & Defense
      • Sci-Tec
      • SpaceX
      • Satish Dhawan Space Centre SHAR
      • True Anomaly
      • Turion Space

Spacecraft Intention Recognition

Author: CislunarSpace

Site: https://cislunarspace.cn

Definition

Spacecraft Intention Recognition is the process of inferring the purpose or mission of a target spacecraft by analyzing its orbital motion behavior, carried equipment types, environmental lighting and electromagnetic conditions, and other multi-source information. It is an important research direction in Space Situational Awareness (SSA) and space safety early warning, aiming to provide threat assessment and decision support for operational spacecraft.

Traditional space threat assessment primarily relies on geometric indicators such as minimum distance, which cannot distinguish the true intent of a target. Spacecraft intention recognition elevates threat assessment from "whether it is approaching" to "why it is approaching."

Intention Classification Framework

Jing et al. (2025) proposed an intention classification framework in the context of space station operational safety, categorizing intentions into 3 major types and 23 subtypes. Note: This is one proposed classification scheme in the academic literature, not a universally accepted standard.

Motion Intentions

Describe the orbital motion pattern of the target spacecraft relative to the operational spacecraft:

IntentionDescription
HoveringTarget maintains constant relative distance with zero relative velocity
FlybyRelative distance decreases then increases, but never reaches zero
FlyaroundRelative distance is non-zero, fluctuating within a narrow range
RendezvousBoth relative distance and velocity reach zero
CollisionRelative distance is zero with non-zero relative velocity
RetreatTarget that previously collided maneuvers away
RandomnessIntent is unclear or time-varying

Operation Intentions

Describe specific operational actions the target spacecraft may perform:

IntentionDescription
DockingStructural connection via robotic arm or docking mechanism
RefuelingFuel injection into the operational spacecraft
RepairReplacement or addition of equipment parts
GrabbingAttachment to operational spacecraft via robotic arm or flying claw
PhotographClose-range photography of operational spacecraft via camera
CommunicationElectromagnetic signal transmission to operational spacecraft

Task Intentions

Combine motion and operation intentions to describe the overall mission purpose:

IntentionDescription
DetectionNoncooperative target, hovering + flyaround, photograph + information gathering
SurveillanceCooperative target, similar to detection but with cooperative nature
InterferenceNoncooperative target, hovering + rendezvous + flyaround, grabbing + electromagnetic interference
NegotiationHovering + flyaround, communication
ObservationSimilar to detection but without operation intentions
AssistanceCooperative target, rendezvous + repair
DeterrenceNoncooperative target, repeatedly executing multiple motion intentions
SupportCooperative target, hovering + flyaround, no operation intentions
ExperimentCooperative target, carrying experimental equipment
AttackNoncooperative target, collision, no operation intentions

LLM-Based Recognition Method

Jing et al. (2025) proposed a spacecraft intention recognition method based on Large Language Models (LLMs). The core idea is to convert multi-source sensor information into text input and leverage the logical reasoning capabilities of LLMs for intent assessment.

Method Framework

  1. Intention vocabulary construction: Define 3 categories and 23 intention terms forming a spacecraft intention corpus
  2. Prompt element design: Extract scene information into 4 categories and 7 prompt elements (operational spacecraft info, target info, environmental conditions, orbital motion characteristics)
  3. Prompt template design: Construct standardized input templates based on prompt engineering principles
  4. Test sample generation: Generate 50,688 nominal samples and 8,448 perturbed samples via computer simulation
  5. Model fine-tuning: Fine-tune ChatGLM2-6B and ChatGLM3-6B using P-tuning V2 and LoRA

Prompt Strategies

Three prompt conditions were tested:

  • Basic prompt: Contains only the question and known information
  • Instruction prompt: Adds all possible answer options to the basic prompt, with instructions guiding the LLM to select from them
  • Chain-of-Thought (CoT) prompt: Requires the LLM to output its reasoning process, including instruction, reasoning steps, and examples

Experimental Results

ModelPrompt TypeAccuracy
ChatGLM2-6B base modelBasic/Instruction/CoTLow (<50%)
ChatGLM2-6B + P-tuning V2CoT99.81%
ChatGLM3-6B base modelCoTBetter than ChatGLM2-6B
ChatGLM3-6B + LoRAInstruction99.90%

Fine-tuned models improved accuracy by 58.66%–83.94% over base models, though robustness decreased.

Applications

  • Space station safety early warning: Identifying the intent of noncooperative targets approaching a space station to support avoidance decisions
  • Space situational awareness: Beyond cataloging on-orbit objects, further determining their behavioral purposes
  • On-orbit servicing planning: Understanding the status of cooperative/noncooperative targets to assist service mission design
  • Space security: Assessing potential threat target intentions in military scenarios

Related Concepts

  • Noncooperative Target
  • Clohessy-Wiltshire (CW) Equation
  • Chain-of-Thought (CoT) Prompting
  • Low-Rank Adaptation (LoRA)
  • Prompt Tuning (P-tuning)
  • Space Traffic Management (STM)

References

  • Jing H, Sun Q, Dang Z, Wang H. Intention Recognition of Space Noncooperative Targets Using Large Language Models. Space Sci. Technol. 2025;5:0271.
  • Sun Q, Dang Z. Deep neural network for non-cooperative space target intention recognition. Aerosp Sci Technol. 2023;142:108681.
  • Yang Z, Shi P, Zhou T, Li W-L. Intention recognition method of space non-cooperative target based on fuzzy reasoning. J Beijing Univ Aeronaut Astronaut. 2024.
  • Qi P, et al. A method and system for intent analysis of non cooperative target spacecraft. Patent 202310735989.X, 2023.
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Last Updated: 6/3/26, 12:52 PM
Contributors: Hermes Agent, Cron Job, Ou Yang Jiahong
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