ESS Power - Power Distribution
The ESS Power component is the central authority for distributing active and reactive power across all battery ESS units in an OpenEMS Edge system. Every control cycle, it collects power requests from all active controllers, resolves any conflicts, respects each ESS’s hardware limits, and delivers a consistent setpoint to each unit.
It follows the OpenEMS Input-Process-Output model: hardware measurements are read first, controllers add their constraints, and the computed setpoints are written to the ESS units - all within a single cycle.
1. Control Cycle
The power distribution runs every Core cycle (1 second default), aligned with the OpenEMS Edge cycle events:
- AfterProcessImage
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Live measurements are captured from each ESS: allowed charge power, allowed discharge power, state-of-charge, and maximum apparent power. These values define the hardware boundaries for the upcoming solve and remain constant for the rest of the cycle.
- BeforeWrite
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Controllers inject their power requests as constraints. The solver computes a setpoint for each ESS and calls
applyPower()on each ESS. - AfterWrite
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Constraints are cleared. Fresh constraints will be collected at the start of the next cycle.
The process image — including hardware limits — is guaranteed not to change between AfterProcessImage and AfterWrite.
Controllers always work against a consistent image of the system state.
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2. Power Constraints
A constraint is a bound that a controller places on the power of a specific ESS for the current cycle. Multiple controllers can add constraints simultaneously; the solver finds the ESS setpoint that satisfies all of them at once.
| Type | Meaning | Example |
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Force an exact power value |
Charge this ESS at exactly 5 000 W |
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Set an upper limit |
Discharge no more than 10 000 W |
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Set a lower limit |
Must discharge at least 2 000 W |
Constraints can apply to:
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Active power (W) — real power delivered to or drawn from the Grid
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Reactive power (VAr) — reactive power for power factor or voltage support
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All phases combined (symmetric ESS) or individual phases L1 / L2 / L3 (asymmetric ESS)
Example: A peak-shaving controller sets a LESS_OR_EQUALS constraint to cap grid feed-in.
At the same time, an emergency reserve controller sets a GREATER_OR_EQUALS constraint to ensure a minimum SoC buffer is never discharged.
The solver satisfies both simultaneously; if they conflict, it finds the closest feasible operating point and raises a fault flag.
If the set of constraints has no feasible solution, all ESS units are driven to zero for that cycle and the NotSolved channel is set.
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2.1 Coefficients
A Coefficient identifies the specific power quantity being targeted by a constraint. It answers three questions:
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Which ESS? — the ESS or cluster by ID
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Which power type? — active power (W) or reactive power (VAr)
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Which phase? — all phases combined (symmetric) or a single phase L1 / L2 / L3 (asymmetric)
For example: "the active power of ESS1 across all phases" is one Coefficient. "the reactive power of ESS2 on phase L2" is another.
Simple Constraints
A simple constraint binds a single Coefficient to a fixed value. This is what controllers typically use to express a power request:
ESS1 / All phases / Active power <= 10 000 W
Complex Constraints
A complex constraint ties two or more Coefficients together in a linear relationship. No fixed value is imposed — instead, a ratio between the power quantities of different ESS units is enforced. This is what the distribution strategies use internally to express proportional loading:
ESS1_ActivePower x weight_B = ESS2_ActivePower x weight_A
Example: The Move Towards Target strategy builds one such constraint for every pair of ESS units. If ESS1 should carry 70 % and ESS2 should carry 30 % of the total power, the constraint becomes:
ESS1_ActivePower x 30 = ESS2_ActivePower x 70
The solver satisfies this alongside all hardware and controller constraints simultaneously, producing a setpoint where both the ratio and the bounds are respected.
| Controllers always use simple constraints. Complex constraints are constructed internally by the solver strategies and are never exposed to individual controllers. |
3. Solvers
The component provides two types solver. The active solver is selected by the strategy configuration parameter.
| Engine | Strategy | Best suited for |
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V1 — Linear Constraint Solver |
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Systems with multiple standalone ESS units where SoC balancing and constraint-based optimisation are required |
V2 — Balance |
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Clustered systems where physical ESS units are grouped under a MetaEss and proportional top-down distribution is sufficient |
4. V1 — Linear Constraint Solver
V1 uses linear programming to find the optimal power setpoint for each ESS that satisfies all active constraints simultaneously.
If the chosen strategy cannot produce a valid setpoint, the engine automatically tries the remaining strategies in the fallback order defined below.
As a final last resort, ALL_CONSTRAINTS performs a pure feasibility solve — finding any operating point that satisfies all hardware and controller constraints, with no further optimisation objective.
| Configured strategy | Fallback sequence (left to right, then ALL_CONSTRAINTS) |
|---|---|
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→ |
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→ |
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→ |
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→ |
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→ |
4.1 Charge / Discharge Direction
Before distributing power, the engine determines the operating direction from the combined effect of all active constraints:
- DISCHARGE
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Power flows out of the battery into the grid or load.
- CHARGE
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Power flows into the battery from the grid or a PV source.
- KEEP_ZERO
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No power exchange is required. All ESS units are driven toward zero active power.
4.2 ESS Selection
When only a subset of ESS units is needed to fulfil a power request, the engine activates the minimum number required:
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On discharge: ESS units with the highest state-of-charge are activated first.
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On charge: ESS units with the lowest state-of-charge are activated first.
This reduces unnecessary cycling of units that do not need to participate in a given operating point and limits wear on ESS units that are already near their SoC limits.
Example: Three batteries at 80 %, 60 %, and 30 % SoC must deliver 10 kW. If one ESS alone can cover 10 kW, only the 80 % unit is used. The other two remain idle for that cycle.
| The operating direction does not switch immediately when the power request changes from discharge to charge or vice versa. The engine waits for 100 consecutive cycles of the new direction before committing to the switch. This prevents rapid ESS on/off switching when the system oscillates around zero power. |
4.3 Distribution Strategies
4.3.1 Move Towards Target
Each ESS is assigned a weight derived from its state-of-charge and the current operating direction:
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Discharge: weight is proportional to SoC — higher SoC ESS units carry more of the load.
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Charge: weight is inversely proportional to SoC — lower SoC ESS units absorb more of the incoming power.
Rather than jumping immediately to the target weights, the distribution moves 10 % of the remaining difference each cycle. This produces a smooth, gradual load shift between ESS units and avoids abrupt step changes on the AC bus.
Example: Two batteries at 70 % and 40 % SoC must discharge 8 kW. The target weight gives 70 % of the power (~5.6 kW) to the high-SoC unit and 30 % (~2.4 kW) to the low-SoC unit. If last cycle both were carrying equal power, this cycle moves 10 % of the way toward that split. Over the following cycles, the distribution gradually converges to the SoC-weighted target.
4.3.2 Keep Target Direction and Maximize in Order
Each active ESS is pushed as far as possible in the target direction — full discharge or full charge — one ESS at a time — on discharge, highest SoC first; on charge, lowest SoC first. The first ESS is loaded to its hardware limit before the next one is engaged.
This strategy minimises the number of ESS units operating simultaneously and runs each participating unit at or near its rated power rather than spreading a modest load across all units.
4.3.3 Keep All Equal
All active ESS units carry the same active and reactive power. Power is split equally regardless of state-of-charge.
This is appropriate when all battery units are identical in capacity and chemistry, and even thermal loading across ESS units is the primary objective.
| If strict equality is not achievable under the individual hardware limits (e.g. one ESS is near its charge limit), the strategy falls back to Keep All Near Equal automatically. |
4.3.4 Keep All Near Equal (default)
Power is distributed using SoC-based weights, computed in the same way as Move Towards Target:
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Discharge: weight proportional to SoC — higher SoC ESS units carry more of the load.
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Charge: weight inversely proportional to SoC — lower SoC ESS units absorb more of the incoming power.
Unlike Move Towards Target, which shifts gradually toward the target over many cycles, Keep All Near Equal solves the weighted distribution in one step each cycle using a linear system (LU decomposition). The proportionality equations and the total power sum are expressed as a matrix and solved directly to produce each ESS’s setpoint.
If the unconstrained solution would push any ESS beyond its hardware limit, that ESS is clamped to its limit and the remaining power is redistributed among the unclamped units — still proportionally, using the same SoC weights. This clamping and re-solve repeats until all ESS setpoints are within their bounds.
Example: Two ESS units must discharge 8 kW. ESS A has SoC 60 % and can deliver up to 6 kW; ESS B has SoC 40 % and can deliver up to 10 kW. The initial weighted split gives ESS A ~5.3 kW (60 %) and ESS B ~3.7 kW (40 %). Since both are within their limits, the result is applied directly — no clamping needed. If the target were instead 12 kW, the weighted split would give ESS A ~7.2 kW — exceeding its 6 kW limit. ESS A is clamped to 6 kW and the remaining 6 kW is assigned entirely to ESS B, which has sufficient headroom.
ESS units currently in a fault state are automatically excluded and held at zero active power. This prevents a faulted unit from reducing the total available capacity and starving healthy ESS units of their fair share.
4.3.5 All Constraints
ALL_CONSTRAINTS performs a pure feasibility solve with no optimisation objective.
Rather than balancing SoC or distributing power proportionally, it simply finds any operating point that satisfies all active hardware and controller constraints simultaneously.
It is used in two ways:
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As an explicit configuration choice — when no distribution optimisation is needed, the solver skips all strategy logic and goes directly to the feasibility solve.
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As the automatic last-resort fallback — after every other configured strategy has failed to produce a valid solution,
ALL_CONSTRAINTSis always tried before the solver gives up and sets all ESS units to zero.
4.4 Reactive Power
In V1, reactive power is solved jointly with active power in the same linear constraint system. Controller constraints on reactive power are added alongside active power constraints and satisfied simultaneously in a single solve.
The apparent power limit is enforced inside the solver — not as a post-solve check.
Before each cycle, the apparent power circle (P² + Q² ≤ S²) is approximated by 8 linear tangent lines forming a polygon, and these are injected as hardware constraints alongside the AllowedCharge and AllowedDischarge bounds.
The solver physically cannot produce a P+Q combination that lies outside this polygon.
The polygon approximation is slightly conservative — the octagon sits inside the true circle — so the usable apparent power is marginally less than the rated value. In V2, by contrast, reactive power is bounded sequentially after active power is fixed, using the exact formula Q_max = sqrt(S² - P²).
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5. V2 — Balance
V2 is used when a cluster groups several physical ESS units under a single logical ESS (MetaEss). It does not use linear programming — instead, power is distributed top-down through the cluster hierarchy in a single pass.
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The cluster receives a target setpoint from its constraint (e.g. charge the entire cluster at 20 kW).
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The target is clamped to the aggregate charge or discharge capability of all member ESS units. This clamping happens before distribution begins — so if the target is physically unreachable, each ESS still receives a valid, feasible command rather than an impossible one.
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Power is divided among members proportionally to their individual available capacity. The reason for proportional distribution is the same as in Keep All Near Equal: an ESS with more headroom can and should absorb a larger share, making full use of the available capacity across the cluster.
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Sub-clusters are resolved recursively in the same way, level by level, until every physical ESS has a setpoint.
Each ESS’s contribution is bounded by its own allowed charge or discharge power at every level. Infeasible cluster targets — for example, requesting more power than all members combined can provide — are automatically corrected to the nearest achievable value before distribution begins.
5.1 Reactive Power
In V2, reactive power is solved after active power. Once each ESS’s active power setpoint is fixed, its remaining reactive power capacity is calculated from the apparent power rating:
Q_max = sqrt( Apparent_power^2 - Active_power^2 )
The reactive power setpoint is then bounded to [-Q_max .. +Q_max], and any controller constraints — such as a target reactive power — are applied within that window.
This guarantees that the combined active and reactive setpoint never exceeds the ESS’s apparent power rating Apparent_power, regardless of the active power share.
6. Output Filtering
To prevent rapid oscillations in the power command sent to hardware, each ESS’s setpoint is passed through an output filter before being applied. The filter type is selected in the configuration.
- PID Filter (default)
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A Proportional-Integral-Derivative filter. Reacts quickly to large setpoint changes while dampening small oscillations. This is the recommended setting for most installations.
Default gains: P = 0.3, I = 0.3, D = 0. - PT1 Filter
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A first-order lag filter. The output approaches the target exponentially with a configurable time constant. Simpler than PID and predictable in response speed. Suitable when a fixed ramp rate is preferred over adaptive control.
- Disabled
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No filtering. The raw solver setpoint is written to the inverter each cycle. Use only if ramp-rate limiting is already handled at the inverter or controller level.
| The filter operates per ESS. A system with three batteries uses three independent filter instances, one for each ESS. |
7. Configuration
| Parameter | Default | Description |
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Power distribution strategy (see section 3) |
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Forces asymmetric ESS units to balance all three phases to the same power level |
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Logs active constraints and solver result to the Edge log each cycle |
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Enables PID output filter |
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PID proportional gain |
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PID integral gain |
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PID derivative gain |
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Enables PT1 filter (only effective when PID is disabled) |
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PT1 time constant — time for the output to reach ~63 % of a step change |
8. Status Channels
| Channel | Meaning |
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The hardware limits alone — before any controller constraints — already form an infeasible combination. Indicates a configuration or hardware problem. |
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No valid setpoint could be computed this cycle. All ESS units were set to zero. |
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Time taken by the solver in milliseconds. Useful for performance monitoring. |
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The strategy that successfully produced a solution this cycle. Helps identify when fallbacks are being used regularly. |