System managing orbital module movement around parent entities. More...

#include <OrbitalSystem.hpp>

Inheritance diagram for ecs::OrbitalSystem:

Collaboration diagram for ecs::OrbitalSystem:

Public Member Functions
	OrbitalSystem ()=default
	Default constructor.

	~OrbitalSystem () override=default
	Default destructor.

void	update (Registry &registry, float deltaTime) override
	Updates all orbital module positions.

ComponentMask	getComponentMask () const override
	Gets the component mask for this system.

Public Member Functions inherited from ecs::ISystem
virtual	~ISystem ()=default
	Virtual destructor.

Private Member Functions
void	updateOrbitalPosition (Registry &registry, Address moduleEntity, OrbitalModule &orbital, Transform &transform, float deltaTime)
	Updates a single orbital module's position.

Detailed Description

System managing orbital module movement around parent entities.

Updates positions of entities with OrbitalModule components to orbit around their parent entities. Uses circular motion with constant radius. Requires OrbitalModule and Transform components.

Definition at line 23 of file OrbitalSystem.hpp.

Constructor & Destructor Documentation

◆ OrbitalSystem()

ecs::OrbitalSystem::OrbitalSystem ( )

default

Default constructor.

◆ ~OrbitalSystem()

ecs::OrbitalSystem::~OrbitalSystem ( )

overridedefault

Default destructor.

Member Function Documentation

◆ getComponentMask()

ComponentMask ecs::OrbitalSystem::getComponentMask ( ) const

overridevirtual

Gets the component mask for this system.

Returns: ComponentMask requiring OrbitalModule and Transform components

Implements ecs::ISystem.

Definition at line 72 of file OrbitalSystem.cpp.

Referenced by update().

◆ update()

void ecs::OrbitalSystem::update	(	Registry &	registry,
		float	deltaTime
	)

overridevirtual

Updates all orbital module positions.

Updates all orbital modules for the current frame.

For each orbital module:

Finds parent entity position
Updates orbital angle based on speed and deltaTime
Calculates new position using circular motion

Parameters

registry	Reference to the ECS registry
deltaTime	Time elapsed since last frame (in seconds)

Implements ecs::ISystem.

Definition at line 18 of file OrbitalSystem.cpp.

References ecs::Registry::getComponent(), getComponentMask(), ecs::Registry::getEntitiesWithMask(), and updateOrbitalPosition().

Here is the call graph for this function:

◆ updateOrbitalPosition()

void ecs::OrbitalSystem::updateOrbitalPosition	(	Registry &	registry,
		Address	moduleEntity,
		OrbitalModule &	orbital,
		Transform &	transform,
		float	deltaTime
	)

private

Updates a single orbital module's position.

Parameters

registry	Reference to the ECS registry
moduleEntity	Entity ID of the orbital module
orbital	OrbitalModule component
transform	Transform component to update
deltaTime	Time elapsed since last frame

Definition at line 32 of file OrbitalSystem.cpp.

References ecs::Registry::getComponent(), ecs::OrbitalModule::getCurrentAngle(), ecs::OrbitalModule::getOrbitRadius(), ecs::OrbitalModule::getOrbitSpeed(), ecs::OrbitalModule::getParentEntityId(), ecs::Transform::getPosition(), ecs::Registry::hasComponent(), LOG_DEBUG, ecs::Registry::setComponent(), ecs::OrbitalModule::setCurrentAngle(), and ecs::Transform::setPosition().