𝔗𝔥𝔢 𝔪𝔦𝔰𝔰𝔦𝔩𝔢 𝔨𝔫𝔬𝔴𝔰 𝔴𝔥𝔢𝔯𝔢 𝔦𝔱 𝔦𝔰 𝔞𝔱 𝔞𝔩𝔩 𝔱𝔦𝔪𝔢𝔰. ℑ𝔱 𝔨𝔫𝔬𝔴𝔰 𝔱𝔥𝔦𝔰 𝔟𝔢𝔠𝔞𝔲𝔰𝔢 𝔦𝔱 𝔨𝔫𝔬𝔴𝔰 𝔴𝔥𝔢𝔯𝔢 𝔦𝔱 𝔦𝔰𝔫'𝔱. 𝔅𝔶 𝔰𝔲𝔟𝔱𝔯𝔞𝔠𝔱𝔦𝔫𝔤 𝔴𝔥𝔢𝔯𝔢 𝔦𝔱 𝔦𝔰 𝔣𝔯𝔬𝔪 𝔴𝔥𝔢𝔯𝔢 𝔦𝔱 𝔦𝔰𝔫'𝔱, 𝔬𝔯 𝔴𝔥𝔢𝔯𝔢 𝔦𝔱 𝔦𝔰𝔫'𝔱 𝔣𝔯𝔬𝔪 𝔴𝔥𝔢𝔯𝔢 𝔦𝔱 𝔦𝔰 (𝔴𝔥𝔦𝔠𝔥𝔢𝔳𝔢𝔯 𝔦𝔰 𝔤𝔯𝔢𝔞𝔱𝔢𝔯), 𝔦𝔱 𝔬𝔟𝔱𝔞𝔦𝔫𝔰 𝔞 𝔡𝔦𝔣𝔣𝔢𝔯𝔢𝔫𝔠𝔢, 𝔬𝔯 𝔡𝔢𝔳𝔦𝔞𝔱𝔦𝔬𝔫. 𝔗𝔥𝔢 𝔤𝔲𝔦𝔡𝔞𝔫𝔠𝔢 𝔰𝔲𝔟𝔰𝔶𝔰𝔱𝔢𝔪 𝔲𝔰𝔢𝔰 𝔡𝔢𝔳𝔦𝔞𝔱𝔦𝔬𝔫𝔰 𝔱𝔬 𝔤𝔢𝔫𝔢𝔯𝔞𝔱𝔢 𝔠𝔬𝔯𝔯𝔢𝔠𝔱𝔦𝔳𝔢 𝔠𝔬𝔪𝔪𝔞𝔫𝔡𝔰 𝔱𝔬 𝔡𝔯𝔦𝔳𝔢 𝔱𝔥𝔢 𝔪𝔦𝔰𝔰𝔦𝔩𝔢 𝔣𝔯𝔬𝔪 𝔞 𝔭𝔬𝔰𝔦𝔱𝔦𝔬𝔫 𝔴𝔥𝔢𝔯𝔢 𝔦𝔱 𝔦𝔰 𝔱𝔬 𝔞 𝔭𝔬𝔰𝔦𝔱𝔦𝔬𝔫 𝔴𝔥𝔢𝔯𝔢 𝔦𝔱 𝔦𝔰𝔫'𝔱, 𝔞𝔫𝔡 𝔞𝔯𝔯𝔦𝔳𝔦𝔫𝔤 𝔞𝔱 𝔞 𝔭𝔬𝔰𝔦𝔱𝔦𝔬𝔫 𝔴𝔥𝔢𝔯𝔢 𝔦𝔱 𝔴𝔞𝔰𝔫'𝔱, 𝔦𝔱 𝔫𝔬𝔴 𝔦𝔰. ℭ𝔬𝔫𝔰𝔢𝔮𝔲𝔢𝔫𝔱𝔩𝔶, 𝔱𝔥𝔢 𝔭𝔬𝔰𝔦𝔱𝔦𝔬𝔫 𝔴𝔥𝔢𝔯𝔢 𝔦𝔱 𝔦𝔰, 𝔦𝔰 𝔫𝔬𝔴 𝔱𝔥𝔢 𝔭𝔬𝔰𝔦𝔱𝔦𝔬𝔫 𝔱𝔥𝔞𝔱 𝔦𝔱 𝔴𝔞𝔰𝔫'𝔱, 𝔞𝔫𝔡 𝔦𝔱 𝔣𝔬𝔩𝔩𝔬𝔴𝔰 𝔱𝔥𝔞𝔱 𝔱𝔥𝔢 𝔭𝔬𝔰𝔦𝔱𝔦𝔬𝔫 𝔱𝔥𝔞𝔱 𝔦𝔱 𝔴𝔞𝔰, 𝔦𝔰 𝔫𝔬𝔴 𝔱𝔥𝔢 𝔭𝔬𝔰𝔦𝔱𝔦𝔬𝔫 𝔱𝔥𝔞𝔱 𝔦𝔱 𝔦𝔰𝔫'𝔱.

ℑ𝔫 𝔱𝔥𝔢 𝔢𝔳𝔢𝔫𝔱 𝔱𝔥𝔞𝔱 𝔱𝔥𝔢 𝔭𝔬𝔰𝔦𝔱𝔦𝔬𝔫 𝔱𝔥𝔞𝔱 𝔦𝔱 𝔦𝔰 𝔦𝔫 𝔦𝔰 𝔫𝔬𝔱 𝔱𝔥𝔢 𝔭𝔬𝔰𝔦𝔱𝔦𝔬𝔫 𝔱𝔥𝔞𝔱 𝔦𝔱 𝔴𝔞𝔰𝔫'𝔱, 𝔱𝔥𝔢 𝔰𝔶𝔰𝔱𝔢𝔪 𝔥𝔞𝔰 𝔞𝔠𝔮𝔲𝔦𝔯𝔢𝔡 𝔞 𝔳𝔞𝔯𝔦𝔞𝔱𝔦𝔬𝔫, 𝔱𝔥𝔢 𝔳𝔞𝔯𝔦𝔞𝔱𝔦𝔬𝔫 𝔟𝔢𝔦𝔫𝔤 𝔱𝔥𝔢 𝔡𝔦𝔣𝔣𝔢𝔯𝔢𝔫𝔠𝔢 𝔟𝔢𝔱𝔴𝔢𝔢𝔫 𝔴𝔥𝔢𝔯𝔢 𝔱𝔥𝔢 𝔪𝔦𝔰𝔰𝔦𝔩𝔢 𝔦𝔰, 𝔞𝔫𝔡 𝔴𝔥𝔢𝔯𝔢 𝔦𝔱 𝔴𝔞𝔰𝔫'𝔱. ℑ𝔣 𝔳𝔞𝔯𝔦𝔞𝔱𝔦𝔬𝔫 𝔦𝔰 𝔠𝔬𝔫𝔰𝔦𝔡𝔢𝔯𝔢𝔡 𝔱𝔬 𝔟𝔢 𝔞 𝔰𝔦𝔤𝔫𝔦𝔣𝔦𝔠𝔞𝔫𝔱 𝔣𝔞𝔠𝔱𝔬𝔯, 𝔦𝔱 𝔱𝔬𝔬 𝔪𝔞𝔶 𝔟𝔢 𝔠𝔬𝔯𝔯𝔢𝔠𝔱𝔢𝔡 𝔟𝔶 𝔱𝔥𝔢 𝒢𝐸𝒜. ℌ𝔬𝔴𝔢𝔳𝔢𝔯, 𝔱𝔥𝔢 𝔪𝔦𝔰𝔰𝔦𝔩𝔢 𝔪𝔲𝔰𝔱 𝔞𝔩𝔰𝔬 𝔨𝔫𝔬𝔴 𝔴𝔥𝔢𝔯𝔢 𝔦𝔱 𝔴𝔞𝔰. 𝔗𝔥𝔢 𝔪𝔦𝔰𝔰𝔦𝔩𝔢 𝔤𝔲𝔦𝔡𝔞𝔫𝔠𝔢 𝔠𝔬𝔪𝔭𝔲𝔱𝔢𝔯 𝔰𝔠𝔢𝔫𝔞𝔯𝔦𝔬 𝔴𝔬𝔯𝔨𝔰 𝔞𝔰 𝔣𝔬𝔩𝔩𝔬𝔴𝔰. 𝔅𝔢𝔠𝔞𝔲𝔰𝔢 𝔞 𝔳𝔞𝔯𝔦𝔞𝔱𝔦𝔬𝔫 𝔥𝔞𝔰 𝔪𝔬𝔡𝔦𝔣𝔦𝔢𝔡 𝔰𝔬𝔪𝔢 𝔬𝔣 𝔱𝔥𝔢 𝔦𝔫𝔣𝔬𝔯𝔪𝔞𝔱𝔦𝔬𝔫 𝔱𝔥𝔢 𝔪𝔦𝔰𝔰𝔦𝔩𝔢 𝔥𝔞𝔰 𝔬𝔟𝔱𝔞𝔦𝔫𝔢𝔡, 𝔦𝔱 𝔦𝔰 𝔫𝔬𝔱 𝔰𝔲𝔯𝔢 𝔧𝔲𝔰𝔱 𝔴𝔥𝔢𝔯𝔢 𝔦𝔱 𝔦𝔰. ℌ𝔬𝔴𝔢𝔳𝔢𝔯, 𝔦𝔱 𝔦𝔰 𝔰𝔲𝔯𝔢 𝔴𝔥𝔢𝔯𝔢 𝔦𝔱 𝔦𝔰𝔫'𝔱, 𝔴𝔦𝔱𝔥𝔦𝔫 𝔯𝔢𝔞𝔰𝔬𝔫, 𝔞𝔫𝔡 𝔦𝔱 𝔨𝔫𝔬𝔴𝔰 𝔴𝔥𝔢𝔯𝔢 𝔦𝔱 𝔴𝔞𝔰. ℑ𝔱 𝔫𝔬𝔴 𝔰𝔲𝔟𝔱𝔯𝔞𝔠𝔱𝔰 𝔴𝔥𝔢𝔯𝔢 𝔦𝔱 𝔰𝔥𝔬𝔲𝔩𝔡 𝔟𝔢 𝔣𝔯𝔬𝔪 𝔴𝔥𝔢𝔯𝔢 𝔦𝔱 𝔴𝔞𝔰𝔫'𝔱, 𝔬𝔯 𝔳𝔦𝔠𝔢-𝔳𝔢𝔯𝔰𝔞, 𝔞𝔫𝔡 𝔟𝔶 𝔡𝔦𝔣𝔣𝔢𝔯𝔢𝔫𝔱𝔦𝔞𝔱𝔦𝔫𝔤 𝔱𝔥𝔦𝔰 𝔣𝔯𝔬𝔪 𝔱𝔥𝔢 𝔞𝔩𝔤𝔢𝔟𝔯𝔞𝔦𝔠 𝔰𝔲𝔪 𝔬𝔣 𝔴𝔥𝔢𝔯𝔢 𝔦𝔱 𝔰𝔥𝔬𝔲𝔩𝔡𝔫'𝔱 𝔟𝔢, 𝔞𝔫𝔡 𝔴𝔥𝔢𝔯𝔢 𝔦𝔱 𝔴𝔞𝔰, 𝔦𝔱 𝔦𝔰 𝔞𝔟𝔩𝔢 𝔱𝔬 𝔬𝔟𝔱𝔞𝔦𝔫 𝔱𝔥𝔢 𝔡𝔢𝔳𝔦𝔞𝔱𝔦𝔬𝔫 𝔞𝔫𝔡 𝔦𝔱𝔰 𝔳𝔞𝔯𝔦𝔞𝔱𝔦𝔬𝔫, 𝔴𝔥𝔦𝔠𝔥 𝔦𝔰 𝔠𝔞𝔩𝔩𝔢𝔡 𝔢𝔯𝔯𝔬𝔯.