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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
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      • 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)
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      • Low Prograde Orbit (LoPO)
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      • Lyapunov Orbit
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      • Parking Orbit
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      • 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

Chain-of-Thought (CoT) Prompting

Author: CislunarSpace

Site: https://cislunarspace.cn

Definition

Chain-of-Thought (CoT) Prompting is a prompt engineering technique proposed by Wei et al. (2022) that encourages Large Language Models (LLMs) to generate a series of intermediate reasoning steps before producing a final answer, rather than jumping directly to the conclusion. This approach significantly improves LLM performance on complex tasks requiring multi-step logical reasoning.

Core Structure

A complete CoT prompt typically comprises three elements:

  1. Instruction: Specifies the task objective and desired output format
  2. Rationale: The intermediate reasoning process, including solutions, inference steps, and relevant external knowledge
  3. Exemplars: Few-shot input-output pairs, each consisting of a question, the reasoning process, and the corresponding answer

How It Works

CoT works by providing a small number of examples with explicit reasoning chains in the prompt, teaching the model to generate similar step-by-step reasoning when processing new questions.

For example, in a spacecraft intention recognition task, a CoT prompt example might be:

Input: The target continuously approaches our space station, reaches the closest distance, then gradually moves away. The target is a large cooperative spacecraft equipped with an operating robotic arm. Lighting condition is full sunlight; electromagnetic condition is optimal.

Output: The target continuously approaches us, reaches the closest distance, then gradually moves away. The inferred Movement Intention is flyby; the target is a large cooperative satellite with a robotic arm, and inferred Operation Intention is refuel; based on this information, the Task intention is unclear.

When facing new inputs, the model mimics this reasoning format, analyzing observation data first and then progressively deriving intentions at each level.

Performance Characteristics

  • Scales with model size: As model parameters increase, CoT answer accuracy progressively improves
  • Outperforms standard prompts: In most domains, CoT accuracy exceeds standard prompting methods
  • Exceeds human performance in some domains: In certain areas (e.g., sports knowledge), CoT accuracy surpasses human performance
  • Interpretability: The reasoning process output provides a traceable path for model decisions

Limitations

  • Unknown mechanism: No universally accepted theory explains why CoT improves model reasoning ability
  • Small model challenges: CoT effectiveness may be limited on smaller models with fewer than 10B parameters (though fine-tuning can mitigate this)
  • Unstable reasoning quality: Generated reasoning may contain errors or irrelevant steps

Variants and Extensions

  • Self-Consistency: Wang et al. (2022) proposed using multiple sampling and majority voting to improve CoT answer accuracy
  • Least-to-Most Prompting: Zhou et al. (2022) proposed first decomposing complex problems into subproblems, then solving each sequentially with CoT
  • Zero-shot CoT: Simply appending "Let's think step by step" to the prompt triggers reasoning chains without providing examples

Application in Spacecraft Intention Recognition

In the study by Jing et al. (2025), CoT was used to enhance LLM reasoning capabilities for spacecraft intention recognition. By providing examples with reasoning processes in CoT prompts, the model learned to first analyze orbital motion patterns and target characteristics, then progressively derive motion intentions, operation intentions, and task intentions. Experiments showed that the CoT-prompt-fine-tuned ChatGLM2-6B model achieved 99.81% accuracy on the intention recognition task.

Related Concepts

  • Prompt Tuning (P-tuning)
  • Spacecraft Intention Recognition
  • Low-Rank Adaptation (LoRA)

References

  • Wei J, Wang X, Schuurmans D, et al. Chain-of-thought prompting elicits reasoning in large language models. Adv Neural Inform Proc Syst. 2022;35:24824-24837.
  • Wang X, Wei J, Schuurmans D, et al. Self-consistency improves chain of thought reasoning in language models. arXiv:2203.11171, 2022.
  • Zhou D, Schärli N, Hou L, et al. Least-to-most prompting enables complex reasoning in large language models. arXiv:2205.10625, 2022.
  • Jing H, Sun Q, Dang Z, Wang H. Intention Recognition of Space Noncooperative Targets Using Large Language Models. Space Sci. Technol. 2025;5:0271.
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Last Updated: 6/3/26, 12:52 PM
Contributors: Hermes Agent, Cron Job, Ou Yang Jiahong
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