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20. Space Mission Planning

Archived At most quadratic

QAOA heuristic, at most quadratic advantage. Classical trajectory optimizers mature. Archived per Troyer framework.

Algorithm
QAOA Trajectory Optimization
Logical Qubits
3
Framework
Modern QDK (qsharp 1.27+)

Resource Estimation (Azure Quantum RE)

Physical Qubits
157.5k
Logical Qubits
12
T-Gates
0
Rotations
9
Runtime
277.2μs

Resource Breakdown

Calibration Evidence (20-Run Ensemble)

Mean Value
0.000
95% CI
± 0.000
Runs
20
Std Dev
0.000

Noise Resilience (Depolarizing Simulation)

Ideal outcome: [Zero, Zero, Zero] (45% probability)

p = 0.001
95.9%
p = 0.01
96.5%
p = 0.05
89.0%

Cross-Platform Emulator Results (100 shots)

Quantinuum H2-1E
[1, 0, 1]
35% of shots
Rigetti QVM
[0, 0, 0]
45% of shots
H2-1E Distribution
Rigetti QVM Distribution

Troyer Utility-Scale Classification

Heuristic / Unproven Advantage
Quantum Speedup
None proven
Classical Competitor
Dynamic programming / genetic algorithms
Honest Assessment (Troyer Framework)

Trajectory optimization is well-served by classical methods. QAOA for routing/scheduling has the same unproven-advantage limitations as other combinatorial optimization problems.

Multi-Model Resource Comparison

Physical qubit requirements across 6 qubit technologies × 2 QEC schemes (inspired by Troyer Architecture Series, Part 3).

■ Gate-based + Surface (blue)■ Majorana + Surface (green)■ Majorana + Floquet (light green)
Qubit ModelQECPhysical QubitsLogical Qubits
Trapped Ion (μs, 1e-4)surface_code70012
Trapped Ion (μs, 1e-3)surface_code2,26812
Majorana (ns, 1e-6)surface_code8,85612
Superconducting (ns, 1e-4)surface_code24,60012
Majorana (ns, 1e-6) (Floquet)floquet_code31,82412
Superconducting (ns, 1e-3)surface_code157,46412
Majorana (ns, 1e-4)surface_code631,94412
Majorana (ns, 1e-4) (Floquet)floquet_code853,34412

Problem Documentation

Problem 20 · Quantum Space Mission Planning

Overview

Designing efficient interplanetary trajectories involves balancing launch windows, gravity assists, and propulsive maneuvers under tight mission constraints. This scaffold couples a reproducible classical baseline based on patched-conic transfer approximations with a Q# project prepared for future quantum annealing and amplitude amplification studies. The objective is to benchmark classical delta-v budgets and schedule feasibility against quantum-inspired search strategies for complex mission profiles.

Directory Layout


20_space_mission_planning/
├── estimates/                        # JSON artifacts from classical and quantum workflows
├── instances/                        # Mission geometries, gravity assist sequences, and time budgets
├── plots/                            # Generated figures from analyze.py
├── python/
│   ├── classical_baseline.py         # Patched-conic delta-v estimator and window feasibility scoring
│   └── analyze.py                    # Visualization of delta-v breakdowns and schedule slack
└── qsharp/
    ├── qsharp.json            # Modern QDK project file
    └── Program.qs                    # Stubbed quantum workflow

Quick Start


cd problems/20_space_mission_planning

# Classical mission baseline
python python/classical_baseline.py

# Plot delta-v budgets and schedule slack
python python/analyze.py

# Quantum placeholder (uses modern QDK  qsharp Python package)
python -c "import qsharp; qsharp.init(project_root='qsharp'); print('Build OK')"
 python tooling/run_all_qsharp.py  # runs via qsharp Python package

Next Quantum Milestones

1. Trajectory Encoding – Map transfer legs into qubit registers for annealing or amplitude amplification.

2. Constraint Encoding – Incorporate launch windows, gravity assists, and vehicle limits via penalty functions.

3. Hybrid Heuristics – Combine classical patched-conic seeding with quantum search refinement.

4. Resource Estimation – Evaluate qubit counts and circuit depth for realistic mission complexity.

This scaffold keeps the classical planning baseline reproducible while preparing for quantum-enhanced mission optimization.

Objective Maturity Gate

  • **Current gate**: **Stage B complete** (classical baseline and Q# scaffold/build path are in place).
  • **Next gate target**: **Stage C** (hardware-aware validation with uncertainty-bounded comparisons).

Stage C exit criteria for this problem:

  • Execute at least one non-placeholder quantum workflow path tied to the problem objective.
  • Report uncertainty-bounded comparisons between classical and quantum outputs on `small` and `medium` instances.
  • Document transpilation/connectivity and backend assumptions used for reported quantum runs.
  • Add calibration/noise-sensitivity evidence for the reported quantum metrics.

DiVincenzo Readiness (Stage C/D Overlay)

| Criterion | Status | Evidence / Notes |

|---|---|---|

| Scalable qubit system | partial | Problem-scoped instance baselines are in place; full hardware-scale projections are tracked as Stage C work. |

| Initialization | partial | Input/state initialization path is defined for current workflows, with backend-ready loading fidelity still to be hardened. |

| Coherence vs gate time | not-yet | Backend-calibrated coherence-vs-depth evidence is pending and required for Stage C/D promotion. |

| Universal gate set | partial | Q# scaffold/build path exists; gate-basis decomposition and transpilation evidence remain Stage C tasks. |

| Qubit-specific measurement | partial | Measurement outputs are defined for current validation flows; hardware readout characterization is pending. |

Advantage Claim Contract

  • **Claim category (current)**: `theoretical`.
  • **Problem class and regime**: Problem-specific challenge instances defined in this directory.
  • **Fair baseline**: Problem-local classical baseline in `python/` outputs.
  • **Quantum resource scaling claim**: Expected asymptotic advantage depends on algorithm family and implementation assumptions; no hardware-demonstrated speedup claim yet.
  • **Data-loading and I/O assumptions**: Must be documented alongside future advantage claims.
  • **Noise/error model assumptions**: Backend-specific model and calibration assumptions to be added at Stage C.
  • **Confidence/uncertainty method**: To be reported using shot-based confidence intervals or equivalent statistical bounds.
  • **Residual risks**: Oracle/state-preparation/transpilation overhead may dominate for near-term instance sizes.

Reproduce It

cd problems/20_space_mission_planning make classical # Run classical baseline make analyze # Generate plots make build # Validate Q# compilation make run # Run Q# entry point

Key Files

  • qsharp/src/Main.qs Quantum algorithm implementation
  • qsharp/HardwareKernel.qs Azure-submittable QIR kernel
  • python/classical_baseline.py Classical reference implementation
  • estimates/classical_baseline.json Baseline metrics
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