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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
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      • Frozen Orbit
      • Gaussian Perturbation Equations
      • Geocentric Inertial Frame
      • GPS Time
      • Gravitational Potential
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      • Gravity Turn
      • Gravity vs Gravitation
      • High Altitude Airship (HAA)
      • Hit Equation
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      • Instantaneous Balance Assumption
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      • Julian Date
      • Kepler's Equation
      • Korea Multi-Purpose Satellite (KOMPSAT)
      • Lagrangian Perturbation Equations
      • Launch Azimuth
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      • Lift-to-Drag Ratio
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      • Longitudinal and Lateral Motion
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      • Near-space
      • Newton's Iteration Method
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      • Perturbation Motion
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      • Reentry Corridor
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      • Repeat Ground Track Orbit
      • Reusable Launch Vehicle
      • Synthetic Aperture Radar (SAR)
      • Satellite Ring
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      • Solar Exposure Factor
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      • Subsatellite Track
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      • Thrust-to-Weight Ratio
      • Thrust
      • Total Angle of Attack
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      • 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
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      • Coasting Arc (Coasting Arc)
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      • Cooperative Agent (CA)
      • CR3BP with Low-Thrust (CR3BP-LT)
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      • Hamiltonian
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      • Invariant Manifold (Invariant Manifold)
      • J2000 Geocentric Equatorial Coordinate System (J2000 Geocentric Equatorial Coordinate System)
      • Jacobi Constant (Jacobi Integral)
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      • Lindstedt-Poincare Method (Lindstedt-Poincare Method)
      • L2-centered Rotating Coordinate System (L2-centered Rotating Coordinate System, LRC)
      • LSTM Neural Network
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      • Mass Discontinuity (Mass Discontinuity)
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      • State Transition Matrix (STM)
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      • Zero-Effort Miss (ZEM)
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    • Mission orbits

      • Apolune
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    • Navigation & systems

      • Altitude Regulation
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    • Astronomy & observation

      • Astrometry
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    • Military space doctrine

      • Anti-Satellite Test (ASAT)
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      • Operational Test and Training Infrastructure (OTTI)
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      • Space Domain Awareness (SDA)
      • Space Mission Task Force (SMTF)
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      • 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

Observability

Author: Tianjiang Shuo

Reference: Qian Yingjing (2014), "Research on Autonomous Navigation and Orbit Keeping of Spacecraft on Quasi-Periodic Orbits in Cislunar Space"

Website: https://cislunarspace.cn

Definition

Observability is a core concept in systems theory and control theory, describing the degree to which the internal states of a system can be determined through external output (measurement) information. In navigation system design, observability analysis is used to determine: given a set of sensor configurations and measurement information, whether the system states can be uniquely and accurately estimated.

For autonomous navigation systems, observability analysis is a critical step in navigation scheme design. A navigation system that fails to satisfy observability requirements cannot provide convergent state estimates, even with an optimal filtering algorithm.

Observability of Linear Systems

Definition

For a linear time-invariant system:

x˙=Ax+Bu\dot{\mathbf{x}} = \mathbf{A}\mathbf{x} + \mathbf{B}\mathbf{u} x˙=Ax+Bu

y=Cx+Du\mathbf{y} = \mathbf{C}\mathbf{x} + \mathbf{D}\mathbf{u} y=Cx+Du

its observability matrix is:

O=[CCACA2⋮CAn−1]\mathcal{O} = \begin{bmatrix} \mathbf{C} \\ \mathbf{C}\mathbf{A} \\ \mathbf{C}\mathbf{A}^2 \\ \vdots \\ \mathbf{C}\mathbf{A}^{n-1} \end{bmatrix} O=​CCACA2⋮CAn−1​​

where nnn is the state dimension. The necessary and sufficient condition for complete observability is rank(O)=n\text{rank}(\mathcal{O}) = nrank(O)=n.

Observability Criteria

CriterionConditionApplicable Scenario
Rank criterionrank(O)=n\text{rank}(\mathcal{O}) = nrank(O)=nGeneral linear systems
GRAM criterionOTO\mathcal{O}^T\mathcal{O}OTO is positive definiteContinuous systems
PBH criterionrank[sI−A,C]=n,∀s\text{rank}[s\mathbf{I}-\mathbf{A}, \mathbf{C}] = n, \forall srank[sI−A,C]=n,∀sLinear systems

Observability of Nonlinear Systems

Locally Weak Observability

For a nonlinear system:

x˙=f(x)\dot{\mathbf{x}} = \mathbf{f}(\mathbf{x}) x˙=f(x)

y=h(x)\mathbf{y} = h(\mathbf{x}) y=h(x)

the locally weakly observable criterion can be applied. The system is locally weakly observable in a neighborhood if and only if:

rank(∂∂xLkh(x))=n,∀k≥0,∀x\text{rank}\left(\frac{\partial}{\partial \mathbf{x}} \mathcal{L}^k h(\mathbf{x})\right) = n, \forall k \geq 0, \forall \mathbf{x} rank(∂x∂​Lkh(x))=n,∀k≥0,∀x

where Lkh\mathcal{L}^k hLkh is the kkk-th Lie derivative of hhh.

Degree of Observability

In practical engineering, even when a system satisfies the observability criteria, state estimation accuracy may still be poor due to insufficient information content. The degree of observability is used to quantify this "level of observability":

obs=σmin⁡σmax⁡\text{obs} = \frac{\sigma_{\min}}{\sigma_{\max}} obs=σmax​σmin​​

where σmin⁡\sigma_{\min}σmin​ and σmax⁡\sigma_{\max}σmax​ are the minimum and maximum singular values of the observability matrix, respectively. A degree of observability closer to 1 indicates that all state components can be estimated with similar ease; a degree closer to 0 indicates that certain state components are difficult to estimate.

Applications in Navigation System Design

Sensor Configuration Optimization

Observability analysis is used to optimize sensor configuration. When studying Sun-Earth-Moon-based autonomous navigation, Qian Yingjing (2014) compared three sensor configuration schemes through observability analysis:

  1. Scheme 1: Sun sensor + Earth sensor + Moon sensor
  2. Scheme 2: Star tracker + Sun/Earth sensor combination
  3. Scheme 3: Optical camera + image processing

The analysis results showed significant differences in the degree of observability among the different configuration schemes, requiring the optimal configuration to be selected based on mission requirements.

Sampling Strategy Optimization

Observability is closely related to observation arc length. Longer continuous observation arcs generally provide better observability but increase computational burden and response latency. In practical design, a balance must be struck between observability and system real-time performance.

Navigation Filter Design

Observability analysis results directly influence filter design:

  • For system state components with poor observability, prior information or constraints need to be added
  • For unobservable states, reduced-order filters or fixed-value treatment should be employed

Limitations of Observability Analysis

  1. Local nature: Locally weak observability analysis only guarantees local uniqueness; global observability is difficult to determine
  2. Model dependence: Analysis results depend on the accuracy of the system dynamics model
  3. Numerical stability: Observability matrix computation for high-dimensional systems may suffer from numerical ill-conditioning
  4. Time-varying systems: Observability analysis of time-varying systems is more complex

Related Concepts

  • Autonomous Navigation
  • Sun-Earth-Moon Autonomous Navigation (SEM Navigation)
  • Extended Kalman Filter (EKF)
  • State Transition Matrix (STM)

References

  • Hermann R, Krener A J. Nonlinear controllability and observability [J]. IEEE Transactions on Automatic Control, 1977.
  • Qian Yingjing. Research on Autonomous Navigation and Orbit Keeping of Spacecraft on Quasi-Periodic Orbits in Cislunar Space [D]. Harbin Institute of Technology, 2014.
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Last Updated: 6/5/26, 9:33 AM
Contributors: Ou Yang Jiahong
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