Ejemplo n.º 1
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	def set_orbit(self, e1, e2, distance, angle_in_degrees, clockwise=True):
		pc1 = self.manager.get_entity_comp(e1, PhysicsEcsComponent.name())
		pc2 = self.manager.get_entity_comp(e2, PhysicsEcsComponent.name())

		if pc1 == None or pc2 == None:
			return

		# TODO what if we want to orbit from where we are? ie no angle specified
		rad = math.radians(angle_in_degrees)
		x = pc2.pos.x + distance * math.cos(rad)
		y = pc2.pos.y + distance * math.sin(rad)
		pc1.pos.x = x
		pc1.pos.y = y

		gv = (pc1.pos - pc2.pos).normalized()
		ov = vec2d.vec2d(gv.y, gv.x)

		if clockwise:
			ov.y *= -1
		else:
			ov.x *= -1

		mag = math.sqrt((GRAV_CONSTANT * pc2.mass) / distance)
		ov *= mag
		pc1.vel = ov
		pc1.acc = vec2d.vec2d(0, 0) # make acceleration zero
Ejemplo n.º 2
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    def set_orbit(self, e1, e2, distance, angle_in_degrees, clockwise=True):
        pc1 = self.manager.get_entity_comp(e1, PhysicsEcsComponent.name())
        pc2 = self.manager.get_entity_comp(e2, PhysicsEcsComponent.name())

        if pc1 == None or pc2 == None:
            return

        # TODO what if we want to orbit from where we are? ie no angle specified
        rad = math.radians(angle_in_degrees)
        x = pc2.pos.x + distance * math.cos(rad)
        y = pc2.pos.y + distance * math.sin(rad)
        pc1.pos.x = x
        pc1.pos.y = y

        gv = (pc1.pos - pc2.pos).normalized()
        ov = vec2d.vec2d(gv.y, gv.x)

        if clockwise:
            ov.y *= -1
        else:
            ov.x *= -1

        mag = math.sqrt((GRAV_CONSTANT * pc2.mass) / distance)
        ov *= mag
        pc1.vel = ov
        pc1.acc = vec2d.vec2d(0, 0)  # make acceleration zero
Ejemplo n.º 3
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 def __init__(self, x, y, mass, static=False, vx=0.0, vy=0.0):
     super(PhysicsEcsComponent, self).__init__()
     self.pos = vec2d.vec2d(x, y)
     self.vel = vec2d.vec2d(vx, vy)
     self.acc = vec2d.vec2d(0, 0)
     self.mass = float(mass)
     self.static = static
Ejemplo n.º 4
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	def __init__(self, x, y, mass, static=False, vx=0.0, vy=0.0):
		super(PhysicsEcsComponent, self).__init__()
		self.pos = vec2d.vec2d(x, y)
		self.vel = vec2d.vec2d(vx, vy)
		self.acc = vec2d.vec2d(0, 0)
		self.mass = float(mass)
		self.static = static
Ejemplo n.º 5
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    def update(self, dt):
        player_sys = self.manager.get_system(player.PlayerEscSystem.name())

        phys_comp_list = self.manager.comps[phys.PhysicsEcsComponent.name()]
        coll_comp_list = self.manager.comps[collision.CollisionEcsComponent.name()]
        aster_comp_list = self.manager.comps[AsteroidEcsComponent.name()]

        # generate
        if player_sys.player_entity_id:
            player_pc = self.manager.get_entity_comp(player_sys.player_entity_id, phys.PhysicsEcsComponent.name())
            player_sc = self.manager.get_entity_comp(player_sys.player_entity_id, ship.ShipEcsComponent.name())
            if player_pc and player_sc:
                time = player_sys.time_limit
                if time % 20 == 0:

                    if player_pc.vel.length > random.randint(1, phys.SPEED_LIMIT):

                        player_angle = player_pc.vel.get_angle()
                        gen_angle = random.choice(
                            [angle for angle in range(int(player_angle - 90), int(player_angle + 90))])
                        gen_pos = vec2d.vec2d(self.generate_radius, 0)
                        gen_pos.rotate(gen_angle)
                        gen_pos = player_pc.pos + gen_pos

                        valid_pos = True
                        for idx, physc in enumerate(phys_comp_list):
                            if physc:
                                collc = coll_comp_list[idx]
                                if physc.pos.get_distance(gen_pos) < collc.radius:
                                    valid_pos = False

                        gen_vel = vec2d.vec2d(random.randint(0, 80), random.randint(0, 80))
                        # create new asteroid
                        if valid_pos:
                            self.manager.create_entity([phys.PhysicsEcsComponent(gen_pos.x, gen_pos.y, mass=100,
                                                                                 static=False, vx=gen_vel.x,
                                                                                 vy=gen_vel.y),
                                                        collision.CollisionEcsComponent(radius=14),
                                                        AsteroidEcsComponent(impact_resistance=50.0, health=100),
                                                        RenderAsteroidEcsComponent(img.IMG_ASTER)])

            entities = self.manager.entities
            for idx, eid in enumerate(entities):
                asterc = aster_comp_list[idx]
                if asterc:
                    physc = phys_comp_list[idx]
                    if physc and player_pc:
                        if player_pc.pos.get_distance(physc.pos) > self.generate_radius:
                            self.manager.mark_entity_for_removal(eid)
Ejemplo n.º 6
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	def thrust_forward(self, eid):
		sc = self.manager.get_entity_comp(eid, ShipEcsComponent.name())

		if sc.fuel > 0:
			rsc = self.manager.get_entity_comp(eid, RenderShipEcsComponent.name())
			pc = self.manager.get_entity_comp(eid, phys.PhysicsEcsComponent.name())

			if not sc or not pc: return
			
			dir_radians = math.radians(sc.rotation)
			dirv = vec2d.vec2d(math.cos(dir_radians), math.sin(dir_radians))
			dirv.length = sc.thrust_force

			sc.fuel -= 1	

			pc.apply_force(dirv.x, dirv.y)

			rsc.thrust_started()
		else:
			print 'out of fuel'
Ejemplo n.º 7
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    def thrust_forward(self, eid):
        sc = self.manager.get_entity_comp(eid, ShipEcsComponent.name())

        if sc.fuel > 0:
            rsc = self.manager.get_entity_comp(eid,
                                               RenderShipEcsComponent.name())
            pc = self.manager.get_entity_comp(eid,
                                              phys.PhysicsEcsComponent.name())

            if not sc or not pc: return

            dir_radians = math.radians(sc.rotation)
            dirv = vec2d.vec2d(math.cos(dir_radians), math.sin(dir_radians))
            dirv.length = sc.thrust_force

            sc.fuel -= 1

            pc.apply_force(dirv.x, dirv.y)

            rsc.thrust_started()
        else:
            print 'out of fuel'
Ejemplo n.º 8
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def get_circle_closest_point(pos, cpos, cradius):
	dv = math.sqrt(math.pow(cpos.x - pos.x, 2) + math.pow(cpos.y - pos.y, 2))
	cx = cpos.x + (cradius * (pos.x - cpos.x) / dv)
	cy = cpos.y + (cradius * (pos.y - cpos.y) / dv)

	return vec2d.vec2d(cx, cy)
Ejemplo n.º 9
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	def update(self, dt):
		phys_comp_list = self.manager.comps[phys.PhysicsEcsComponent.name()]
		coll_comp_list = self.manager.comps[CollisionEcsComponent.name()]

		entities_to_remove = set()

		# we use this guy to keep track of the collision 'matrix'
		entity_collision_dict = {}

		entities = self.manager.entities
		for idx, eid in enumerate(entities):
			physc = phys_comp_list[idx]
			collc = coll_comp_list[idx]

			if physc == None or collc == None:
				continue

			for oidx, oeid in enumerate(entities):
				if eid == oeid: continue

				ophysc = phys_comp_list[oidx]
				ocollc = coll_comp_list[oidx]

				if ophysc == None or ocollc == None:
					continue

				d = physc.pos.get_distance(ophysc.pos)
				coll_d = collc.radius + ocollc.radius

				if d <= coll_d: # collision
					e_coll_list = entity_collision_dict.setdefault(eid, [])
					if oeid not in e_coll_list:
						e_coll_list.append(oeid)
						entity_collision_dict.setdefault(oeid, []).append(eid)

						overlap = coll_d - d

						# resolve the collision
						dir = ophysc.pos- physc.pos

						if physc.static:
							dir.length = overlap
							ophysc.pos = ophysc.pos + dir * 2
						elif ophysc.static:
							dir.length = overlap
							physc.pos = ophysc.pos + dir * 2
						else:
							dir.length = overlap / 2
							physc.pos = physc.pos - dir * 2
							ophysc.pos = ophysc.pos + dir * 2

						# calculate reflection here
						ocontact_point = get_circle_closest_point(physc.pos, ophysc.pos, ocollc.radius)
						normal = vec2d.vec2d(ocontact_point.x - ophysc.pos.x, ocontact_point.y - ophysc.pos.y).normalized()

						incidence = (physc.vel) - (ophysc.vel)

						mtotal = physc.mass + ophysc.mass
						c1 = physc.mass / mtotal
						c2 = ophysc.mass / mtotal

						r = incidence - (2 * incidence.dot(normal)) * normal

						impact_size = (ophysc.vel - physc.vel).length

						angle = abs(r.get_angle_between(normal))
					
						if angle > 1:
							#print angle, angle * 0.3
							mod = angle * 0.3

							if r.length > mod:
								r.length -= mod
							else:
								r.length = 0

							#r.length /= (angle * 0.3)

						# friction jobbie
						#j = max(-(1 + 0.1) * physc.vel.dot(normal), 0.0)
						#print j, impact_size
						#r += normal * j

						#contact.rigidBody->linearMomentum += j * contact.normal;

						self.manager.entity_collision(eid, oeid, impact_size, r * c2, CollisionEcsSystem.name(), 'collision')
						self.manager.entity_collision(oeid, eid, impact_size, ~r * c1, CollisionEcsSystem.name(), 'collision')
Ejemplo n.º 10
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 def apply_force(self, x, y):
     force = vec2d.vec2d(x / self.mass, y / self.mass)
     self.vel = self.vel + force
Ejemplo n.º 11
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	def apply_force(self, x, y):
		force = vec2d.vec2d(x / self.mass, y / self.mass)
		self.vel = self.vel + force
Ejemplo n.º 12
0
def get_circle_closest_point(pos, cpos, cradius):
    dv = math.sqrt(math.pow(cpos.x - pos.x, 2) + math.pow(cpos.y - pos.y, 2))
    cx = cpos.x + (cradius * (pos.x - cpos.x) / dv)
    cy = cpos.y + (cradius * (pos.y - cpos.y) / dv)

    return vec2d.vec2d(cx, cy)
Ejemplo n.º 13
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    def update(self, dt):
        phys_comp_list = self.manager.comps[phys.PhysicsEcsComponent.name()]
        coll_comp_list = self.manager.comps[CollisionEcsComponent.name()]

        entities_to_remove = set()

        # we use this guy to keep track of the collision 'matrix'
        entity_collision_dict = {}

        entities = self.manager.entities
        for idx, eid in enumerate(entities):
            physc = phys_comp_list[idx]
            collc = coll_comp_list[idx]

            if physc == None or collc == None:
                continue

            for oidx, oeid in enumerate(entities):
                if eid == oeid: continue

                ophysc = phys_comp_list[oidx]
                ocollc = coll_comp_list[oidx]

                if ophysc == None or ocollc == None:
                    continue

                d = physc.pos.get_distance(ophysc.pos)
                coll_d = collc.radius + ocollc.radius

                if d <= coll_d:  # collision
                    e_coll_list = entity_collision_dict.setdefault(eid, [])
                    if oeid not in e_coll_list:
                        e_coll_list.append(oeid)
                        entity_collision_dict.setdefault(oeid, []).append(eid)

                        overlap = coll_d - d

                        # resolve the collision
                        dir = ophysc.pos - physc.pos

                        if physc.static:
                            dir.length = overlap
                            ophysc.pos = ophysc.pos + dir * 2
                        elif ophysc.static:
                            dir.length = overlap
                            physc.pos = ophysc.pos + dir * 2
                        else:
                            dir.length = overlap / 2
                            physc.pos = physc.pos - dir * 2
                            ophysc.pos = ophysc.pos + dir * 2

                        # calculate reflection here
                        ocontact_point = get_circle_closest_point(
                            physc.pos, ophysc.pos, ocollc.radius)
                        normal = vec2d.vec2d(ocontact_point.x - ophysc.pos.x,
                                             ocontact_point.y -
                                             ophysc.pos.y).normalized()

                        incidence = (physc.vel) - (ophysc.vel)

                        mtotal = physc.mass + ophysc.mass
                        c1 = physc.mass / mtotal
                        c2 = ophysc.mass / mtotal

                        r = incidence - (2 * incidence.dot(normal)) * normal

                        impact_size = (ophysc.vel - physc.vel).length

                        angle = abs(r.get_angle_between(normal))

                        if angle > 1:
                            #print angle, angle * 0.3
                            mod = angle * 0.3

                            if r.length > mod:
                                r.length -= mod
                            else:
                                r.length = 0

                            #r.length /= (angle * 0.3)

                        # friction jobbie
                        #j = max(-(1 + 0.1) * physc.vel.dot(normal), 0.0)
                        #print j, impact_size
                        #r += normal * j

                        #contact.rigidBody->linearMomentum += j * contact.normal;

                        self.manager.entity_collision(
                            eid, oeid, impact_size, r * c2,
                            CollisionEcsSystem.name(), 'collision')
                        self.manager.entity_collision(
                            oeid, eid, impact_size, ~r * c1,
                            CollisionEcsSystem.name(), 'collision')
Ejemplo n.º 14
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def generate_system_data():
    # create some working data
    member_names = [
        'Tamde', 'Yol', 'Trog', 'Mar', 'Een', 'Sila', 'Ado', 'Khem', 'Teim',
        'Tamut', 'Beda', 'Ponni'
    ]
    member_position_angles = [i for i in xrange(0, 360, 40)]
    mass_mod = 10000
    member_padding = 1000
    member_grav_radius = member_padding // 2
    satellite_grav_radius = member_grav_radius // 2
    satellite_orbit_distance = member_grav_radius // 2
    satellite_position_angles = [i for i in xrange(0, 360, 90)]
    planet_imgs = [img.IMG_P_64_1, img.IMG_P_64_2]
    moon_imgs = [
        img.IMG_M_48_1,
    ]

    members = []

    # player ship
    player_ship_data = {
        'type': 'ship',
        'size': 14,
        'mass': 100,
        'rotation': 90.0,
        'rotation_speed': 6.0,
        'thrust_force': 200.0,
        'impact_resistance': 50.0,
        'fuel': 700,
        'passengers': 0,
        'health': 350,
        'orbit_distance': member_grav_radius * .75,
        'orbit_angle': 0,
        'orbit_clockwise': False
    }

    # sun
    members.append({
        'x': 0,
        'y': 0,
        'type': 'sun',
        'img': 'sun.png',
        'name': 'Sol',
        'static': True,
        'size': 128,
        'mass': 128 * mass_mod,
        'grav_radius': member_grav_radius,
        'satellites': [
            player_ship_data,
        ]
    })

    crew_to_rescue = 0

    #planets
    distance = 0
    num_planets = xrange(0, 7)  #7
    for _ in num_planets:
        distance += member_padding

        planet_name = random.choice(member_names)
        member_names.remove(planet_name)

        # generate position
        pos = vec2d.vec2d(0, distance)
        angle = random.choice(member_position_angles)
        pos.rotate(angle)

        # member satellites
        satellites = []
        num_satellites = xrange(0, 2)
        satellite_angle_options = satellite_position_angles[:]
        for _ in num_satellites:
            satelite_angle = random.choice(satellite_angle_options)
            satellite_angle_options.remove(satelite_angle)

            satellites.append({
                'type': 'planet',
                'name': 'Satellite',
                'img': random.choice(moon_imgs),
                'size': 24,
                'mass': 24 * mass_mod,
                'grav_radius': satellite_grav_radius,
                'orbit_distance': satellite_orbit_distance,
                'orbit_angle': satelite_angle,
                'orbit_clockwise': True
            })
        # add one base satellite
        satelite_angle = random.choice(satellite_angle_options)
        satellite_angle_options.remove(satelite_angle)
        crew = 30
        crew_to_rescue += 30
        satellites.append({
            'type': 'base',
            'name': 'Satellite',
            'img': img.IMG_BASE,
            'size': 14,
            'mass': 300,
            'service_radius': 65,
            'fuel': True,
            'repair': True,
            'crew': crew,
            'impact_resistence': 70,
            'health': 800,
            'orbit_distance': satellite_orbit_distance,
            'orbit_angle': satelite_angle,
            'orbit_clockwise': True
        })
        members.append({
            'x': pos.x,
            'y': pos.y,
            'type': 'planet',
            'img': random.choice(planet_imgs),
            'name': planet_name,
            'static': True,
            'size': 64,
            'mass': 64 * mass_mod,
            'grav_radius': member_grav_radius,
            'satellites': satellites
        })

    data = {
        'members': members,
        'crew_to_rescue': crew_to_rescue,
    }

    return data
Ejemplo n.º 15
0
def generate_system_data():
	# create some working data
	member_names = ['Tamde', 'Yol', 'Trog', 'Mar', 'Een', 'Sila', 'Ado', 'Khem', 'Teim', 'Tamut', 'Beda', 'Ponni']
	member_position_angles = [i for i in xrange(0, 360, 40)]
	mass_mod = 10000
	member_padding = 1000
	member_grav_radius = member_padding // 2
	satellite_grav_radius = member_grav_radius // 2
	satellite_orbit_distance = member_grav_radius // 2
	satellite_position_angles = [i for i in xrange(0, 360, 90)]
	planet_imgs = [img.IMG_P_64_1, img.IMG_P_64_2]
	moon_imgs = [img.IMG_M_48_1,]

	members = []

	# player ship
	player_ship_data = {'type': 'ship',
		'size': 14,
		'mass': 100,
		'rotation': 90.0,
		'rotation_speed': 6.0,
		'thrust_force': 200.0,
		'impact_resistance': 50.0,
		'fuel': 700,
		'passengers': 0,
		'health': 350,
		'orbit_distance': member_grav_radius * .75,
		'orbit_angle': 0,
		'orbit_clockwise': False
	}

	# sun
	members.append({'x': 0, 'y':0,
			'type': 'sun',
			'img': 'sun.png',
			'name':'Sol',
			'static': True,
			'size': 128,
			'mass': 128 * mass_mod,
			'grav_radius': member_grav_radius,
			'satellites': [player_ship_data,]
		})

	crew_to_rescue = 0

	#planets 
	distance = 0
	num_planets = xrange(0, 7) #7
	for _ in num_planets:
		distance += member_padding

		planet_name = random.choice(member_names)
		member_names.remove(planet_name)

		# generate position
		pos = vec2d.vec2d(0, distance)
		angle = random.choice(member_position_angles)
		pos.rotate(angle)

		# member satellites
		satellites = []
		num_satellites = xrange(0, 2)
		satellite_angle_options = satellite_position_angles[:]
		for _ in num_satellites:
			satelite_angle = random.choice(satellite_angle_options)
			satellite_angle_options.remove(satelite_angle)

			satellites.append({'type': 'planet',
				'name':'Satellite',
				'img': random.choice(moon_imgs),
				'size': 24,
				'mass': 24 * mass_mod,
				'grav_radius': satellite_grav_radius,
				'orbit_distance': satellite_orbit_distance,
				'orbit_angle': satelite_angle,
				'orbit_clockwise': True
			})
		# add one base satellite
		satelite_angle = random.choice(satellite_angle_options)
		satellite_angle_options.remove(satelite_angle)
		crew = 30
		crew_to_rescue += 30
		satellites.append({'type': 'base',
			'name':'Satellite',
			'img': img.IMG_BASE,
			'size': 14,
			'mass': 300,
			'service_radius': 65,
			'fuel': True,
			'repair': True,
			'crew': crew,
			'impact_resistence': 70,
			'health': 800,
			'orbit_distance': satellite_orbit_distance,
			'orbit_angle': satelite_angle,
			'orbit_clockwise': True
		})
		members.append({'x': pos.x, 'y': pos.y,
			'type': 'planet',
			'img': random.choice(planet_imgs),
			'name': planet_name,
			'static': True,
			'size': 64,
			'mass': 64 * mass_mod,
			'grav_radius': member_grav_radius,
			'satellites': satellites
		})

	data = {
		'members': members,
		'crew_to_rescue': crew_to_rescue,
	}

	return data