Arbitrary motor count

[Lagnesh2003]

Derive motor count from mixing_matrix.shape[-1] instead of hardcoding 4, so the simulator is more generalized.

Changes

• SimState, SimStateDeriv, SimControls (crazyflow/sim/data.py): rotor buffers (rotor_vel, rotor_acc) are now sized by n_motors.
• Sim.init_data and rotor_vel_limits (crazyflow/sim/sim.py): n_motors is derived from mixing_matrix.shape[-1] and threaded through; thrust limits scale with n_motors instead of 4 *.
• rotor_vel_control (crazyflow/sim/functional.py): the per-motor shape assertion now reads the motor count off data.states.rotor_vel instead of asserting a fixed 4.
• action_space (crazyflow/envs/drone_env.py): attitude-mode thrust bounds now scale with n_motors instead of * 4.
• Mellinger controller (crazyflow/control/mellinger/control.py): force_torque2rotor_vel and _attitude2force_torque divide by mixing_matrix.shape[-1] instead of 4; state2attitude now takes mixing_matrix as a keyword-only parameter (auto-bound via load_params/parametrize) instead of hardcoding * 4.
• Added tests/unit/test_arbitrary_motor_count.py: 6 regression tests exercising every changed function directly with a synthetic 6-motor mixing_matrix/SimData, without registering a full hexacopter drone. Verified each test fails against the pre-fix code and passes against the fix.

Fixes #104

Test plan

• pytest -v tests — 656 passed (650 existing + 6 new)
• pytest --markdown-docs ... (doctests/docs examples) — 101 passed
• ruff check crazyflow/ tests/ — clean
• New regression tests confirmed to fail on pre-fix code, pass on fixed code